text
stringlengths
30
4k
source
stringlengths
60
201
Feb 27 2002 Example: Two charges Q q r • If q,Q same sign: – U > 0; we have to do work ‘pushing’ charges together • If q,Q unlike sign: – U < 0; Electric force does work ‘pulling’ charges together Feb 27 2002 Electric Potential • Electric Potential Energy proportional to q • Define V = U/q • Electric Potential V: – ...
https://ocw.mit.edu/courses/8-02x-physics-ii-electricity-magnetism-with-an-experimental-focus-spring-2005/5c48da61d3532b22af63ad3792b99f6b_2_27_2002_edited.pdf
single particle (e.g. electron) small • Often measured in ‘Electron Volt’ [eV] • Energy aquired by particle of charge 10-19 C going through ∆V=1V Velocity v +q + + + + + + + ++ + + d Feb 27 2002 Conductors • E = 0 inside – otherwise charges would move • No charges inside – Gauss • E perpendicular to surface – ot...
https://ocw.mit.edu/courses/8-02x-physics-ii-electricity-magnetism-with-an-experimental-focus-spring-2005/5c48da61d3532b22af63ad3792b99f6b_2_27_2002_edited.pdf
6.012 Electronic Devices and Circuits Comments on Photoconductive Detectors - 9/17/09 Version Photoconductivity was first reported in 1873 by W. Smith [J. Soc. Telegraph Eng., Vol. 2 (1873) p. 31], making it one of the first properties of semiconductors to be studied and exploited. At the same time, some of the new...
https://ocw.mit.edu/courses/6-012-microelectronic-devices-and-circuits-fall-2009/5c58a51e629ef0505139e7a4cf72f2fd_MIT6_012F09_lec03_photo.pdf
arrays for these applications can be made from silicon doped with “deep” donors for which the energy required to ionize the donor corresponds to that of the infrared light of interest. Unlike the column V donors we discussed in class, these donors are not normally ionized at room temperature; it is the incident light...
https://ocw.mit.edu/courses/6-012-microelectronic-devices-and-circuits-fall-2009/5c58a51e629ef0505139e7a4cf72f2fd_MIT6_012F09_lec03_photo.pdf
using layers of different semiconductors whose thicknesses and compositions are chosen to create electrons localized in space much like those associated with a deep donor ion (except that they are localized in planes, not about points in space like donor traditional ions). photoconductor, but in exchange for the inc...
https://ocw.mit.edu/courses/6-012-microelectronic-devices-and-circuits-fall-2009/5c58a51e629ef0505139e7a4cf72f2fd_MIT6_012F09_lec03_photo.pdf
Three Lectures on Organizational Structures • Lecture 1 - Typology of generic organizational architectures – Their advantages and disadvantages • Lecture 2 - Simple models of complexity and flexibility; their relationship to each other for each of the generic architectures • Lecture 3 - Relationships of generic ar...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
• Teams can be very flexible and thus robust to certain “attacks” ; if one member is sick, the others ought to be able to take over their role; they can handle many classes of changes in specs with relative ease • Human teams are relatively small in size – volume of output is limited in scale and scope; 7±2 limits ...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
will have interconnections with nodes at the same layer • Nodes at the same layer usually are at the same level of abstraction – not generally true of tree structures • Layer skipping is not permitted in pure layered forms, but is not too problematic most of the time due to understanding of context (e.g., mathemati...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
AI program that proved theorems in Russell and Whitehead’s “Principia Mathematica”) 13 Layered Hierarchies • Layered structure with three layers and no horizontal interconnections, may connect to any or even all nodes in layer immediately above or below. I believe that layered hierarchies are not well understood ...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
, a root node, 10 nodes, with horizontal (lateral) interconnections 17 Lateral Interconnects in Human Organizations and Industries • Horizontal interconnects rely on and foster cooperation and team work • Such interconnects add to the complexity of each node and the overall system. In human organizations such int...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
polynomials with rational number coefficients) – All of the above, except for automobile platforms, are low power systems – There are very many uses of layered systems in practice in CS, computer engineering, and communications, but layering is usually not taught as a design methodology 21 Performance and Flexibilit...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
accounting firms with senior partners, junior partners and associates) • Universities prior to introduction of research -oriented departments in the 19th century by von Humboldt; there is still memory in universities of this organizational structure (e.g., provost/rector, full professors, associate professors and ...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
the new layer that can generate the new product – Make changes at lower layers than where you started as needed to efficiently implement the new product 28 Networks • There are many types of networks, with differing values for the properties of interest to us, such as flexibility and robustness • Grid networks ca...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
Japan and to a lesser degree Germany and Northern Italy). Karl Marx and Max Weber were German, Freud was Austrian • People can be brought up in either approach and in many others as well • Modern cultures are learning from each other to some degree (e.g., the Toyota production system – lean manufacturing). Thus the ...
https://ocw.mit.edu/courses/esd-342-network-representations-of-complex-engineering-systems-spring-2010/5c5b67ad949c857a0932e37036533a63_MITESD_342S10_lec08.pdf
20.330 / 6.023 / 2.793 Fields, Forces and Flows in Biological Systems Instructors: Jongyoon “Jay” Han and Scott Manalis TOPICS Introduction to electric fields Maxwell’s equations Introduction to fluid flows Transport phenomena in biological systems Electro-quasistatics Electrokinetics Electrophoresis Van der ...
https://ocw.mit.edu/courses/20-330j-fields-forces-and-flows-in-biological-systems-spring-2007/5c643ae047c6ae6f7ecaa1e0855ae03c_lec1.pdf
of its environment? E. Coli trajectory Images removed due to copyright restrictions. See Figs. 1 & 3. Berg, Physics Today 2000 http://www.aip.org/pt/jan00/berg.htm Measuring binding kinetics Surface Plasmon Resonance (Biacore) Courtesy of Biacore. Used with permission. Label-free enables direct readout of Kon an...
https://ocw.mit.edu/courses/20-330j-fields-forces-and-flows-in-biological-systems-spring-2007/5c643ae047c6ae6f7ecaa1e0855ae03c_lec1.pdf
pp. 439 (1999) Brown, T., Leonard, G. A., Booth, E. D., Chambers, J, J Mol Biol 207 pp. 455 (1989) Migratory birds uses magnets for positioning Image removed due to copyright restrictions. Figure 1 in Mora, Cordula V. "Magnetoreception and its Trigeminal Mediation in the Homing Pigeon." Nature 432 (2004): 508-511....
https://ocw.mit.edu/courses/20-330j-fields-forces-and-flows-in-biological-systems-spring-2007/5c643ae047c6ae6f7ecaa1e0855ae03c_lec1.pdf
Debye layer - + - + - + - E v Electrophoresis Dielectrophoresis diffusion Chemical reaction +V0 -V0 +V0 Fick’s law of diffusion Maxwell’s equation Concentration(c) (ρ) Electrophoresis ρ, J : source E and B field Convection Osmosis Electroosmosis Streaming potential (aqueous) medium, Flow velocit...
https://ocw.mit.edu/courses/20-330j-fields-forces-and-flows-in-biological-systems-spring-2007/5c643ae047c6ae6f7ecaa1e0855ae03c_lec1.pdf
Massachusetts Institute of Technology 6.270 Autonomous LEGO Robot Competition IAP 2005: Attack of the Drones Workshop 4 — Code & Sensors I: Basic Control and Robot Skills Wednesday, January 5, and Thursday, January 6, 2005 1 Items to Bring • Handy Board with Expansion Board 2 Reading • Handy Board technical ma...
https://ocw.mit.edu/courses/6-270-autonomous-robot-design-competition-january-iap-2005/5c6455005827275583dca5a9083664f2_4_codesensors1.pdf
File: ~/FILENAME.c • Type your program. Use the Handy Board technical reference for assistance with the various functions. When you are done with your program, type: <Ctrl>-x <Ctrl>-c • You will be prompted as to whether or not to save the file under the previously assigned name. Hit “y”. • You should now return a te...
https://ocw.mit.edu/courses/6-270-autonomous-robot-design-competition-january-iap-2005/5c6455005827275583dca5a9083664f2_4_codesensors1.pdf
connections to the robot are made. When ready, turn it back on to test. 2 Updated January 4, 2005
https://ocw.mit.edu/courses/6-270-autonomous-robot-design-competition-january-iap-2005/5c6455005827275583dca5a9083664f2_4_codesensors1.pdf
MIT OpenCourseWare http://ocw.mit.edu 6.046J / 18.410J Design and Analysis of Algorithms Spring 2015 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.edu/terms.
https://ocw.mit.edu/courses/6-046j-design-and-analysis-of-algorithms-spring-2015/5c6cf10a900ea288d97dce247a9a5a9d_MIT6_046JS15_writtenlec2.pdf
ALPHA DRAFT- For Review Only Space Systems, Policy, and Architecture Research Consortium (SSPARC) Draft 11/4/03 “SSPARC BOOK” MATERIAL for Lecture 3 Prepared by: Hugh McManus Metis Design ---- Draft for evaluation only. Do not distruibute. © 2003 Massachusetts Institute of Technology 11/6/03 1 ALPHA DRAFT- For Review ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
erd, Seth Guikema, Cyrus Jilla, Chris Roberts, Satwik Seshasai, Nirav Shah, Todd Shuman, Tim Spaulding, Dave Stagney, Dan Thunnissen, Myles Walton, Annalisa Wiegel, and Brandon Wood, along with their advisors and committees. Many other students, staff, and undergraduate researchers also contributed. Bill Borer, Kevin R...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
............12 Notes on terminology, requirements, and limits .......................................................15 2.5. Process terminology14..............................................................................................15 On requirements14...............................................................
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
.11. Space Tug attribute–design vector mapping.............................................................49 NOTES AND REFERENCES ..................................................................................................50 5.1. 5.2. 5.3. 5.4. 5.5. 5.6. © 2003 Massachusetts Institute of Technology 11/6/03 3 AL...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
mission success, for national defense and prestige, were the driving motivations. The historical basis for current practices in the aerospace industry, and an analysis of the structural changes that the industry has undergone, are covered in detail in chapters 2 and 3 of the Lean Aerospace Initiative book Lean Enterpri...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
s is slow to adapt a better way to design systems to ensure competitiveness in a rapidly changing world. Current approaches to creating aerospace systems requirements do not adequately consider the full range of possible designs and their associated costs and utilities throughout the development and lifecycle.7 These a...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
possible, maintain management leverage as long as possible, and increase knowledge as quickly as possible, while not increasing costs incurred. In light of the above comments, we would also like it to avoid early a priori design selections, include the preferences of key stakeholders, and increase knowledge specificall...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
product development. The Multi-Attribute Tradespace Exploration (MATE) is a model-based high-level assessment of many possible solutions to the problem to be considered. Ideally, the full sweep of possible solutions to the problem are considered here. The key purpose of this step is to avoid premature concentration on ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Define Attributes Define Utilities Define Design Vector Develop System Model Calculate Utilities Estimate Cost Architecture Trade Space Figure 4 High level description of MATE process The first step is selection and bounding of a “mission concept.” Here, the basic issue to be addressed (i.e. the user needs to be satisf...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
in others (e.g. usefulness, to scientists, of scientific data) it can only be used as a relative metric. In the latter case, interpretation of these metrics is somewhat dangerous—a higher metric is better than a lower one, but a utility of 0.5 may not be “half as good” as a 1.0, nor a 0.99 “only 1% off” from a 1.0. Suc...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
in Space Mission Analysis and Design (SMAD)10) are of appropriate fidelity. Other models may have to be custom-developed for specific applications. These models can be linked to automate, or at least partially automate, the analyses, allowing large design spaces to be analyzed efficiently with commonly available comput...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
cost). This region is referred to as the Pareto front. Designs that are not on the Pareto front are said to be “dominated”—better designs are available at the same or lower cost. Choosing between designs on the Pareto front means making real trades—better utility for greater costs, or trading one desired utility agains...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
proceeds, circumstances can change, or knowledge can be gained that changes perceptions, causing earlier decisions to be called into question. For example, user needs can to shift late in the process, or the choice of attributes or design vector can change based on knowledge gained during analytical model development. ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
tool is tended by a human operator who updates the tool as necessary (e.g. updates a CAD model), makes major design decisions that are input to the tool (e.g. changes the propulsion type), and provides common sense and wisdom unavailable to automated methods (e.g. breaks non-convergent behavior in the iterations). The ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
his or her fingertips. The MATE chair can quantitatively assess the progress of the design not just towards meeting requirements, but towards maximizing the overall utility of the system containing the design. He or she can also help the user/customer translate needs into design changes, and thus steer the design chang...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
6% Propulsion (dry) 2% Structures & Mechanisms 18% Thermal 5% Mating System 27% Figure 8 Typical ICE output: vehicle configuration and mass budget for an electric propulsion orbital transfer vehicle.16 ICE methods can be used for more detailed design studies, up to and including creating hardware drawings and/or CAD...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Massachusetts Institute of Technology 11/6/03 14 ALPHA DRAFT- For Review Only 2.5. Notes on terminology, requirements, and limits Process terminology14 The terminology used for the methods described here is far from stable. In this work, the architectural-level trade space exploration is referred to as MATE, the rapi...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
first step, so it is natural to ask how the current method interacts with the determination of system requirements. The present method can be thought of as a powerful tool for coming up with the right requirements at the right time. It has been noted that current processes are not efficient at coming up with requiremen...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
The present method can aid in understanding flexibility issues through understanding of the trade space. Designs can be specified which can be improved to provide enhanced utility with reasonable expense, risk, and/or need for technology advancement. Limits and Caveats14 The MATE-CON method is a useful tool for archite...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
predictions of re-entry time and location for uncontrolled bodies such as spent satellites. Figure 10 shows the MATE process as carried out for the X-TOS project. The X-TOS project was scoped fairly narrowly—the customer needed a system that could deliver and support a set of three pre-existing instruments designed to ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
the key trades—increased lifetime for either increased altitude (and hence reduced data utility) or increased vehicle weight (and hence cost) for added maneuver fuel. These trades are visible on the Pareto front—short lifetime missions are somewhat cheaper at a penalty in utility. © 2003 Massachusetts Institute of Tech...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
(s) • Diversity of Latitude(s) • Time Spent at Equator • Data Latency Design Vector • Number of Vehicles and Mission Design • Apogee Altitude • Perigee Altitude • Orbit Inclination • Antenna Gain • Communications Architecture • Propulsion Type • Power Type • Maneuver Delta-V Capability System Model • • • Orbit Calc...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
, or moving them. The project was motivated by a general interest in such systems as a national capability, and poor results when proposing such systems for specific missions, without looking at the wider tradespace of possible uses and designs. Figure 12 shows the MATE process as carried out for the SpaceTug project. ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
1) observation and manipulator system mass; (2) propulsion type, and (3) mass of fuel carried. © 2003 Massachusetts Institute of Technology 11/6/03 21 ALPHA DRAFT- For Review Only For the simulations, simple parametric relationships and design rules were used to compute the spacecraft characteristics. These were carri...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
vehicles are not optimal according the MATE analysis; the ICE results (which had difficulty closing because of extreme fuel loads) helped to illustrate why. Finally, a variety of Tender vehicles were designed; some for specific missions and some for generic service; these designs showed that a modular approach to tende...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Biprop Cryo Electric Nuclear Nuclear Monsters Tenders Electric Cruisers 0.2 0.4 0.6 0.8 1.0 Utility (dimensionless) Figure 12 MATE process for SPACE TUG © 2003 Massachusetts Institute of Technology ($M2002 ) 11/6/03 23 ALPHA DRAFT- For Review Only 3. DETAILED DESCRIPTION OF MATE-CON PROCESS The following sect...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
They are intended to provide the reader with ideas for implementation, rather than a rigid template. © 2003 Massachusetts Institute of Technology 11/6/03 24 ALPHA DRAFT- For Review Only 4. IDENTIFYING STAKEHOLDERS, NEEDS, MISSION CONCEPT, AND PROJECT SCOPE The first step is selection and bounding of a “mission concept...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
creating a capability, with the hope that if it exists it will create market demand. In this case, the needs of the interested stakeholders needs to be addressed, as well as the potential needs of future users of the system. The Space Tug project illustrates this case. 4.2. Define System Concept and Scope32 Along with ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
on the other hand, includes a large space of possible solutions, but is scoped in terms of the aspects of the problem to be considered and the level of detail of the solutions to be developed. 4.3. Identify Stakeholders and Decision Makers32 In order to understand the true or potential needs for a system, the people, ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
97), the Customer “is an individual or organization that (1) commission the engineering of a system, or (2) is a prospective purchaser of an end product.” The Customer typically has preferences that balance product performance meeting User needs, cost of the system, and political considerations. This decision maker typ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
13 Stakeholder Framework © 2003 Massachusetts Institute of Technology 11/6/03 27 ALPHA DRAFT- For Review Only 4.4. X TOS Need, Concept and Scope32,35 The X-TOS project was motivated by the need for improved predictions of drag on orbiting bodies. This drag is a strong function of the density of the upper atmosphere, w...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
be optimized to meet those users needs. However, lack of maturity of the drag model and information distribution system precluded modeling of these aspects of the system of systems. Instead, the space segment up to the delivery of data to the ground was modeled, and the system was designed to optimize the delivery of d...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
needs; others may emerge once such a capability exists. Among the potential developers and customers for such as system, there is a need to understand systems that maximize potential usefulness. The mission concept of the Space Tug project was very open: a vehicle or vehicles capable of visiting a variety of orbits in ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
5.1. Introduction32 Defining the trade space is the critical next step in the MATE-CON process. In this step, the user’s (and possibly other stakeholders’) preference space is defined. This preference space will be used to evaluate the members of a design space, which must also be defined now. The preference space con...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
the user. A rough view of this mapping is shown in Figure 16. Two caveats are immediately in order. One is that the choices of attributes and design space define the bounds of the trade space. Incorrect choices will result in a trade space that does not reflect the users true needs, or does not contain the best solutio...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
model in order to understand their effects on the trade space. A will be seen later in this book, constraints can often have unintended negative consequences, driving up costs or precluding good solutions. © 2003 Massachusetts Institute of Technology 11/6/03 33 ALPHA DRAFT- For Review Only 5.3. Defining Attributes32 W...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
tend to be specialized and non-intuitive to the lay-person (and the designer!) and were determined with some difficulty. The Launch System4 and Space Tug attributes are simple and relatively intuitive capabilities of the system, representing the customers’ high-level interest in establishing national assets. The commun...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
particular data sample Diversity of Latitudes Contained in Data Set Time Spent at the Equator: Time per day spent +/- 20 degrees off the equatorial Latency: The elapsed time between the collection of data and the start of transmission Space Based Radar:45 Moving Object Tracking Area: Area in which a moving targets may ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
metrics as possible, while keeping in mind the cognitive limitations in practice. (The human mind can typically only think about 7±2 objects simultaneously.41) The perceived-independent property is important for the utility independence axiom, described below, to hold. (The attributes need only be “perceived” independe...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
place for thinking about what the attributes may look like. Brainstorming with as many stakeholders as possible is a desirable first step. Using standard brainstorming technique, collect many © 2003 Massachusetts Institute of Technology 11/6/03 36 ALPHA DRAFT- For Review Only possible attributes, and try to group simi...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
into question the original choices. These iterations on the attribute definitions require progressively more work, so it is desirable to do the best job possible at each step. Ideally, the attributes would be developed in full cooperation with the user. More typically, after the first interaction, the design team works...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
of technical attributes, usually using very different types of models. The cost estimates may be of considerably lower fidelity than the technical simulations, especially when new concepts are being considered. Finally, cost is a useful independent criterion against which to weigh the advantages and disadvantages of va...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
suffered several of the weaknesses mentioned above. Some are not discriminating, e.g. the pointing accuracy was easily within any reasonable vehicle’s capability. Others where not well posed for quantifying, e.g. time spent in various regions. Others were not functional, e.g. mission lifetime described the lifetime of ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
AFRL model Tech Demo Mission – Latency max and min for demonstration of now-casting capability. © 2003 Massachusetts Institute of Technology 11/6/03 39 ALPHA DRAFT- For Review Only There are some complications even in the final set. The sample altitude is a vector of values (one per data sample!) that must be reduced ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
required a rethinking of the attribute list, although it proved to be relatively minor. The updated attribute list included a quantified response time, in hours, from 1 (best) to 2160, or three months (worst). © 2003 Massachusetts Institute of Technology 11/6/03 40 ALPHA DRAFT- For Review Only 5.6. Defining the Design...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Note that the ATOS vector contains no design vector elements concerning the design of the vehicles themselves; the performance of the swarms are only weakly dependent on the performance of the individual vehicles, so a nominal high-level vehicle design is placed in the constants vector. BTOS has only the highest level ...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
is to create a list from which the actual design vector will be reduced. Typically, design vector variables are descriptions of the form of the solution. For space vehicles, this might include vehicle types, subsystem choices, fuel loads, technologies used. For space systems, this might include orbits, operating and co...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
be checked at a number of fixed values, which must be chosen, while discrete ones (e.g. mission scenario) need to be fully defined and quantified. Updating the design vector Experience has shown that the design vector is the least stable element in the trades space. As the modeling, and even the analysis, progress, des...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
not included. On the other hand, since the altitude and latitude range attributes are taken independently (i.e. the user is not expressing preferences for combinations of altitudes and latitudes) one would immediately choose the argument of perigee to align the line of nodes with line of apsides. Such a selection maxim...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
X-TOS Design Vector Design Variable Altitude of Apogee (km) Altitude of Perigee (km) Levels 200:50:350; 650:300:2000* 150:50:350* Inclination (deg) Total Delta-V (m/s) 0; 30; 70; 90 200:100:1000* Comm. Sys Type Antenna Gain Propulsion Type AFSCN; TDRSS High; Low Chemical; Hall Power Sys Type Solar; Fuel cells Mission S...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
high level. Per the assumptions made at the beginning of the study, only the characteristics of the vehicle were considered. A very wide tradespace was considered, so only the design choices likely to have first order effect on the attributes were considered. The final design vector was: Table 7 Space Tug Design Vector...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
conception of necessary modules for the model. This activity is done in parallel with the proposal and finalization of design variables since it helps prioritize design variables and pare down the proposed list. A technique similar to Quality Function Deployment (QFD, also referred to as the House of Quality) is used t...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
can happen when the team’s physical intuition for the problem (understanding that a design variable should affect the outcome) exceeds their functional intuition (understanding what function of the outcome would vary with the design variable). As this step is informational, the process should be modified to suit the pr...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
p m I l a t o T Attributes Data Lifespan Sample Altitude Diversity of Latitudes Time at Equator Latency Total Cost Total w/Cost 9 9 0 0 3 9 9 0 6 3 21 27 9 0 6 6 0 0 0 0 0 9 0 0 0 9 0 0 0 0 3 9 6 6 21 9 12 39 9 6 6 6 6 30 36 12 12 27 12 15 18 48 0 0 0 0 9 9 3 9 0 0 0 0 9 3 9 9 48 9 27 9 18 9 24 3 36 Figure 17 X-TOS att...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
system choice should have a stronger effect. In hindsight, its effect was diminished by the choice of delta-V as a design variable, instead of a more physical parameter such as fuel load. The power system affects data lifespan through its own lifespan, and latency via its ability to provide sufficient power; this sugge...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Tradespace Exploration with Concurrent Design for Creating Aerospace Systems Requirements,” Master of Science Thesis in Aeronautics and Astronautics, Massachusetts Institute of Technology, June 2002. 2 Ross, A. M., “Multi-Attribute Tradespace Exploration with Concurrent Design as a Value- Centric Framework for Space Sy...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
McManus, H. L., and Warmkessel, J. M., “Creating Advanced Architectures for Space Systems: Emergent Lessons from New Processes,” accepted for publication in the Journal of Spacecraft and Rockets, < Vol and Number TBD)> 10 Larson, W. J., and Wertz, J. R., Space Mission Analysis and Design, 3rd ed., Microcosm Press, El S...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
-6370, Sept. 2003. 16 Figures from McManus, H. L. and Schuman, T. E., “Understanding the Orbital Transfer Vehicle Trade Space,” AIAA Paper 2003-6370, Sept. 2003. 17 Aguilar, J. A., and Dawdy, A., “Scope vs. Detail: The Teams of the Concept Design Center,” 2000 IEEE Aerospace Conference Proceedings, Big Sky, Montana, Ma...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
NPDT – The Next generation Concurrent Design Approach,” EUSEC 2000, 2nd European Systems Engineering Conference, Munich, Germany, Sept. 2000. 24 Oxnevad, K. I., “A Concurrent Design Environment for Designing Space Instruments,” Proceedings of the 9th Thermal and Fluids Analysis Workshop, Ohio Aerospace Institute and NA...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
Diller, N. P., Multi-Attribute Trade Space with Concurrent Design MATE- CON: The MATE Short Book, unpublished. 31 A. Ross, N. Diller, and D. Hastings, Multi-Attribute Tradespace Exploration with Concurrent Design for Space System Conceptual Design, AIAA 2003-1328, 41st Aerospace Sciences Meeting and Exhibit, 6 – 9 Janu...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
’s Thesis in Aeronautics and Astronautics, Massachusetts Institute of Technology, June 2003. 38 Shaw, G. M., Miller, D. W., and Hastings, D. E., “Development of the Quantitative Generalized Information Network Analysis (GINA) Methodology for Satellite Systems,” Journal of Spacecraft and Rockets, Vol. 38, No. 2, 2001, p...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
kessel, J. M., “Multi-Attribute Tradespace Exploration as a Front-End for Effective Space System Design,” Journal of Spacecraft and Rockets, January 2004. 45 Spaulding, Timothy J., “Tools for Evolutionary Acquisition: A Study of Multi-Attribute Tradespace Exploration (MATE) applied to the Space Based Radar (SBR),” Mast...
https://ocw.mit.edu/courses/16-892j-space-system-architecture-and-design-fall-2004/5c7b371feea1c1563d917c1858f58ec7_03010lec3framev5.pdf
8.701 0. Introduction 0.3 Teaching Staff Introduction to Nuclear and Particle Physics Markus Klute - MIT 1 Short Bio - Instructor: Markus Klute Markus Klute joined the MIT Physics Department in April 2009. He received his Diploma and Ph.D from Rheinische Friedrich-Wilhems University, Bonn, Germany in 2004 with re...
https://ocw.mit.edu/courses/8-701-introduction-to-nuclear-and-particle-physics-fall-2020/5c9317e4704966ef8d82f0d4a1a3dc6d_MIT8_701f20_lec0.3.pdf
free time. 4 MIT OpenCourseWare https://ocw.mit.edu 8.701 Introduction to Nuclear and Particle Physics Fall 2020 For information about citing these materials or our Terms of Use, visit: https://ocw.mit.edu/terms.
https://ocw.mit.edu/courses/8-701-introduction-to-nuclear-and-particle-physics-fall-2020/5c9317e4704966ef8d82f0d4a1a3dc6d_MIT8_701f20_lec0.3.pdf
Representing Complexity MIT Student Lecture 6 Discussion � Dynamic Models of Segregation Examine how individual incentives/actions aggregate  • to cause segregation Develop set of rules governing individual preference/ tolerance and • movement Many simplifying assumptions • • Representing the complexity of so...
https://ocw.mit.edu/courses/ids-900-doctoral-seminar-in-engineering-systems-fall-2011/5cb05eb8bb0eaaa7e2df65c5e776db99_MITESD_83F11_lec06_discuss.pdf
models and visualization tools Schelling: “Some of the results are going to be judged impressionistically, and it is • worthwhile to get some idea of the kind of picture or pattern that emerges from a random distribution” (156) Van Ham, van Wijk: ““Providing both detailed information as well as a global • cont...
https://ocw.mit.edu/courses/ids-900-doctoral-seminar-in-engineering-systems-fall-2011/5cb05eb8bb0eaaa7e2df65c5e776db99_MITESD_83F11_lec06_discuss.pdf
simplification? How does one qualify these sorts of simplifications when presenting results to • y y policy makers? Slide 7 Question 3: In socioeconomic systems, how simple is too • simple? By focusing on individual incentives, Schelling divorced a socioeconomic • phenomena from most of its social an...
https://ocw.mit.edu/courses/ids-900-doctoral-seminar-in-engineering-systems-fall-2011/5cb05eb8bb0eaaa7e2df65c5e776db99_MITESD_83F11_lec06_discuss.pdf
Coordinates and Transformations MIT ECCS 6.837 Wojciech Matusik many slides follow Steven Gortler’s book 1 Hierarchical modeling • Many coordinate systems: • Camera • Static scene • car • driver • arm • hand • ... Image courtesy of Gunnar A. Sjögren on Wikimedia Commons. License: CC-BY-SA. This conten...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
to facing East • Express coordinate system changes • e.g. given the driver's location in the coordinate system of the car, express it in the coordinate system of the world 7 Goals for today • Make it very explicit what coordinate system is used • Understand how to change coordinate systems • Understand how...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
for example: ... • which gives us 20 Algebra notation • The are also vectors of the space • They can be expressed in the basis for example: • which gives us 21 Recap, matrix notation • Given the coordinates c in basis the transformed vector has coordinates Mc in 22 Why do we care • We li...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
Linear Isotropic Scaling Translation Reflection Rotation Identity Scaling Shear 30 Plan • Vectors • Points • Homogenous coordinates • Normals 31 Points vs. Vectors • A point is a location • A vector is a motion between two points • Adding vectors is meaningful • going 3km North + 4km East = g...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
9 Linear component • Note how we leave the fourth component alone 40 Translation component • Express translation vector t in the basis 41 Translation 42 Full affine expression Which tells us both how to get a new frame ftM or how to get the coordinates Mc after transformation 43 Questions? 44 ...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
.e. the transformation in a is A-1SA • i.e., from right to left, A takes us from a to f, then we apply S, then we go back to a with A-1 51 Questions? 52 How are transforms combined? Scale then Translate (1,1) (0,0) Scale(2,2) (2,2) Translate(3,1) (5,3) (3,1) (0,0) Use matrix multiplication: p' = T...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
0 3 1 1 Translate then Scale: p' = S ( T p ) = ST p ST = 2 0 0 0 2 0 0 0 1 1 0 0 0 1 0 3 1 1 = 2 0 0 0 2 0 6 2 1 55 Questions? 56 Plan • Vectors • Points • Homogenous coordinates • Normals 57 Forward reference and eye • The fourth ...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
: http://openclipart.org/detail/34051/digicam-by-thesaurus. 62 Perspective in 2D The projected point in homogeneous coordinates (we just added w=1): This image is in the public domain. Source: http://openclipart.org/detail/34051/digicam-by-thesaurus. 63 Perspective in 2D Projectively equivalent This image i...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
is perspective. © source unknown. All rights reserved. This content is excluded from our Creative Commons license. For more information, see http://ocw.mit.edu/help/faq-fair-us e/. This image is in the public domain. Source: http://openclipart.org/detail/34051/digicam-by-thesaurus. 68 Questions? 69 Eye candy: ...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
nOS Object Space World Space 78 Transform Normal like Object? •translation? •rotation? •isotropic scale? •scale? •reflection? •shear? •perspective? 79 Transform Normal like Object? •translation? •rotation? •isotropic scale? •scale? •reflection? •shear? •perspective? 80 Transformation for shear ...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf
Mˉ¹)ᵀ nOS Sometimes denoted Mˉᵀ • But why did nWS = M nOS work for similitudes? • Because for similitude / similarity transforms, (Mˉ¹)ᵀ =λ M • e.g. for orthonormal basis: Mˉ¹ = M ᵀ i.e. (Mˉ¹)ᵀ = M 86 Connections • Not part of class, but cool • “Covariant”: transformed by the matrix • e.g., tangent ...
https://ocw.mit.edu/courses/6-837-computer-graphics-fall-2012/5cbb1bf32a92fad91e8ad6c37a473240_MIT6_837F12_Lec03.pdf