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fcb2819
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Parent(s): 4396455
[add] first commit
Browse files- requirements.txt +3 -2
- src/streamlit_app.py +480 -38
requirements.txt
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@@ -1,3 +1,4 @@
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-
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pandas
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streamlit
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pandas
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plotly
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openai
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src/streamlit_app.py
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@@ -1,40 +1,482 @@
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import
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import
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import streamlit as st
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#
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Edit `/streamlit_app.py` to customize this app to your heart's desire :heart:.
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If you have any questions, checkout our [documentation](https://docs.streamlit.io) and [community
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forums](https://discuss.streamlit.io).
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In the meantime, below is an example of what you can do with just a few lines of code:
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"""
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num_points = st.slider("Number of points in spiral", 1, 10000, 1100)
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num_turns = st.slider("Number of turns in spiral", 1, 300, 31)
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indices = np.linspace(0, 1, num_points)
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theta = 2 * np.pi * num_turns * indices
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radius = indices
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x = radius * np.cos(theta)
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y = radius * np.sin(theta)
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df = pd.DataFrame({
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"x": x,
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"y": y,
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"idx": indices,
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"rand": np.random.randn(num_points),
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})
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st.altair_chart(alt.Chart(df, height=700, width=700)
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.mark_point(filled=True)
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.encode(
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x=alt.X("x", axis=None),
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y=alt.Y("y", axis=None),
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color=alt.Color("idx", legend=None, scale=alt.Scale()),
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size=alt.Size("rand", legend=None, scale=alt.Scale(range=[1, 150])),
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))
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# app.py
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import os
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import time
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import math
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import random
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from datetime import datetime
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import streamlit as st
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import pandas as pd
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import plotly.graph_objects as go
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from openai import OpenAI
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# ----------------------------
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# ページ設定
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# ----------------------------
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st.set_page_config(
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page_title="軌道制御支援AIシステム(PoC開発中)",
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page_icon="🛰️",
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layout="wide"
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)
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# ----------------------------
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# OpenAI client
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# ----------------------------
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api_key = os.getenv("OPENAI_API_KEY")
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client = OpenAI(api_key=api_key) if api_key else None
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# ----------------------------
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# 初期状態
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# ----------------------------
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if "sat_state" not in st.session_state:
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st.session_state.sat_state = {
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"angle_deg": 20.0, # 軌道位置角
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"altitude_km": 540.0,
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"speed_kms": 7.66,
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"battery_pct": 92,
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"temp_c": 24.5,
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"signal_db": 81,
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"mode": "IDLE",
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"health": "NOMINAL",
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"last_event": "初期化完了",
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# 追加: レンジング / 姿勢
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"range_km": 1240.0, # 地上局から衛星までの距離
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"pos_x": 420.0, # 軌道面上の相対位置X
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"pos_y": 160.0, # 軌道面上の相対位置Y
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"yaw_deg": 12.0, # 姿勢 Yaw
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"pitch_deg": -4.0, # 姿勢 Pitch
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"roll_deg": 7.0, # 姿勢 Roll
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}
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if "process_logs" not in st.session_state:
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st.session_state.process_logs = []
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# ----------------------------
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# ユーティリティ
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# ----------------------------
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def call_openai(prompt: str) -> str:
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if client is None:
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return "OPENAI_API_KEY が未設定です。ダミー応答を返します。"
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res = client.responses.create(
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model="gpt-4.1-mini",
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input=prompt,
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)
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return res.output_text
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def update_satellite_state(step_idx: int):
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"""工程ごとに衛星状態を少し変化させる"""
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s = st.session_state.sat_state
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s["angle_deg"] = (s["angle_deg"] + random.uniform(18, 38)) % 360
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theta = math.radians(s["angle_deg"])
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s["altitude_km"] = round(540 + random.uniform(-8, 8), 1)
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s["speed_kms"] = round(7.66 + random.uniform(-0.04, 0.04), 3)
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s["battery_pct"] = max(20, min(100, s["battery_pct"] - random.randint(1, 3)))
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s["temp_c"] = round(24 + random.uniform(-4, 6), 1)
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s["signal_db"] = max(35, min(99, s["signal_db"] + random.randint(-6, 4)))
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# 追加: 軌道位置を簡易更新
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orbit_r = 480
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s["pos_x"] = round(orbit_r * math.cos(theta) + random.uniform(-20, 20), 1)
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s["pos_y"] = round(orbit_r * math.sin(theta) + random.uniform(-20, 20), 1)
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# 追加: 地上局(原点近傍)からの距離レンジング
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gs_x, gs_y = 0.0, -420.0
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s["range_km"] = round(
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math.sqrt((s["pos_x"] - gs_x) ** 2 + (s["pos_y"] - gs_y) ** 2) + random.uniform(-15, 15),
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1
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)
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# 追加: 姿勢角を変化
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s["yaw_deg"] = round((s["yaw_deg"] + random.uniform(-8, 8)), 1)
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s["pitch_deg"] = round(max(-45, min(45, s["pitch_deg"] + random.uniform(-4, 4))), 1)
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s["roll_deg"] = round(max(-45, min(45, s["roll_deg"] + random.uniform(-5, 5))), 1)
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modes = {
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0: "BOOT",
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1: "SENSING",
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2: "ANALYZING",
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3: "UPLINK",
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4: "REPORTING",
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}
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events = {
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0: "衛星起動シーケンス",
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1: "テレメトリ取得中",
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2: "観測データ解析中",
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3: "地上局と通信中",
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4: "ミッション結果反映"
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}
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s["mode"] = modes.get(step_idx, "ACTIVE")
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s["last_event"] = events.get(step_idx, "更新")
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s["health"] = "NOMINAL" if s["signal_db"] >= 50 and s["battery_pct"] >= 30 else "CHECK"
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def make_tracking_figure():
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"""
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右側に出す可視化:
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- 左: 地上局から衛星までのレンジング + 軌道位置
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- 右: 衛星姿勢 (機体向き)
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| 122 |
+
"""
|
| 123 |
+
s = st.session_state.sat_state
|
| 124 |
+
|
| 125 |
+
gs_x, gs_y = 0.0, -420.0
|
| 126 |
+
sat_x, sat_y = s["pos_x"], s["pos_y"]
|
| 127 |
+
|
| 128 |
+
fig = go.Figure()
|
| 129 |
+
|
| 130 |
+
# ----------------------------
|
| 131 |
+
# 左エリア: レンジング / 軌道位置
|
| 132 |
+
# ----------------------------
|
| 133 |
+
# 軌道の目安円
|
| 134 |
+
orbit_x = []
|
| 135 |
+
orbit_y = []
|
| 136 |
+
for d in range(361):
|
| 137 |
+
r = math.radians(d)
|
| 138 |
+
orbit_x.append(480 * math.cos(r))
|
| 139 |
+
orbit_y.append(480 * math.sin(r))
|
| 140 |
+
|
| 141 |
+
fig.add_trace(go.Scatter(
|
| 142 |
+
x=orbit_x,
|
| 143 |
+
y=orbit_y,
|
| 144 |
+
mode="lines",
|
| 145 |
+
name="Reference Orbit",
|
| 146 |
+
line=dict(width=2, dash="dot"),
|
| 147 |
+
))
|
| 148 |
+
|
| 149 |
+
# 地上局
|
| 150 |
+
fig.add_trace(go.Scatter(
|
| 151 |
+
x=[gs_x],
|
| 152 |
+
y=[gs_y],
|
| 153 |
+
mode="markers+text",
|
| 154 |
+
name="Ground Station",
|
| 155 |
+
text=["Ground"],
|
| 156 |
+
textposition="bottom center",
|
| 157 |
+
marker=dict(size=14, symbol="square"),
|
| 158 |
+
))
|
| 159 |
+
|
| 160 |
+
# 衛星
|
| 161 |
+
fig.add_trace(go.Scatter(
|
| 162 |
+
x=[sat_x],
|
| 163 |
+
y=[sat_y],
|
| 164 |
+
mode="markers+text",
|
| 165 |
+
name="Satellite Position",
|
| 166 |
+
text=["🛰️"],
|
| 167 |
+
textposition="middle center",
|
| 168 |
+
marker=dict(size=18),
|
| 169 |
+
))
|
| 170 |
+
|
| 171 |
+
# レンジ線
|
| 172 |
+
fig.add_trace(go.Scatter(
|
| 173 |
+
x=[gs_x, sat_x],
|
| 174 |
+
y=[gs_y, sat_y],
|
| 175 |
+
mode="lines",
|
| 176 |
+
name="Range",
|
| 177 |
+
line=dict(width=3),
|
| 178 |
+
))
|
| 179 |
+
|
| 180 |
+
# レンジ注記
|
| 181 |
+
mid_x = (gs_x + sat_x) / 2
|
| 182 |
+
mid_y = (gs_y + sat_y) / 2
|
| 183 |
+
fig.add_annotation(
|
| 184 |
+
x=mid_x,
|
| 185 |
+
y=mid_y,
|
| 186 |
+
text=f"Range: {s['range_km']} km",
|
| 187 |
+
showarrow=False,
|
| 188 |
+
yshift=12
|
| 189 |
+
)
|
| 190 |
+
|
| 191 |
+
# 位置注記
|
| 192 |
+
fig.add_annotation(
|
| 193 |
+
x=sat_x,
|
| 194 |
+
y=sat_y,
|
| 195 |
+
text=f"Pos({s['pos_x']}, {s['pos_y']})",
|
| 196 |
+
showarrow=True,
|
| 197 |
+
ax=30,
|
| 198 |
+
ay=-30
|
| 199 |
+
)
|
| 200 |
+
|
| 201 |
+
# ----------------------------
|
| 202 |
+
# 右エリア: 姿勢表示
|
| 203 |
+
# ----------------------------
|
| 204 |
+
# 右側に独立した姿勢表示領域を作る
|
| 205 |
+
attitude_center_x = 980
|
| 206 |
+
attitude_center_y = 0
|
| 207 |
+
body_len = 120
|
| 208 |
+
|
| 209 |
+
yaw_rad = math.radians(s["yaw_deg"])
|
| 210 |
+
body_dx = body_len * math.cos(yaw_rad)
|
| 211 |
+
body_dy = body_len * math.sin(yaw_rad)
|
| 212 |
+
|
| 213 |
+
# 機体中心
|
| 214 |
+
fig.add_trace(go.Scatter(
|
| 215 |
+
x=[attitude_center_x],
|
| 216 |
+
y=[attitude_center_y],
|
| 217 |
+
mode="markers+text",
|
| 218 |
+
name="Attitude Center",
|
| 219 |
+
text=["SAT"],
|
| 220 |
+
textposition="middle center",
|
| 221 |
+
marker=dict(size=22, symbol="diamond"),
|
| 222 |
+
))
|
| 223 |
+
|
| 224 |
+
# 機体進行方向(Yaw)
|
| 225 |
+
fig.add_trace(go.Scatter(
|
| 226 |
+
x=[attitude_center_x, attitude_center_x + body_dx],
|
| 227 |
+
y=[attitude_center_y, attitude_center_y + body_dy],
|
| 228 |
+
mode="lines+markers",
|
| 229 |
+
name="Yaw Direction",
|
| 230 |
+
line=dict(width=4),
|
| 231 |
+
marker=dict(size=8),
|
| 232 |
+
))
|
| 233 |
+
|
| 234 |
+
# 簡易ソーラーパドル
|
| 235 |
+
panel_span = 70
|
| 236 |
+
perp_dx = panel_span * math.cos(yaw_rad + math.pi / 2)
|
| 237 |
+
perp_dy = panel_span * math.sin(yaw_rad + math.pi / 2)
|
| 238 |
+
|
| 239 |
+
fig.add_trace(go.Scatter(
|
| 240 |
+
x=[attitude_center_x - perp_dx, attitude_center_x + perp_dx],
|
| 241 |
+
y=[attitude_center_y - perp_dy, attitude_center_y + perp_dy],
|
| 242 |
+
mode="lines",
|
| 243 |
+
name="Solar Panel Axis",
|
| 244 |
+
line=dict(width=6),
|
| 245 |
+
))
|
| 246 |
+
|
| 247 |
+
# 姿勢テキスト
|
| 248 |
+
fig.add_annotation(
|
| 249 |
+
x=attitude_center_x,
|
| 250 |
+
y=attitude_center_y - 170,
|
| 251 |
+
text=(
|
| 252 |
+
f"Yaw: {s['yaw_deg']}°<br>"
|
| 253 |
+
f"Pitch: {s['pitch_deg']}°<br>"
|
| 254 |
+
f"Roll: {s['roll_deg']}°"
|
| 255 |
+
),
|
| 256 |
+
showarrow=False
|
| 257 |
+
)
|
| 258 |
+
|
| 259 |
+
fig.add_annotation(
|
| 260 |
+
x=attitude_center_x,
|
| 261 |
+
y=attitude_center_y + 150,
|
| 262 |
+
text="Attitude",
|
| 263 |
+
showarrow=False,
|
| 264 |
+
font=dict(size=16)
|
| 265 |
+
)
|
| 266 |
+
|
| 267 |
+
fig.update_layout(
|
| 268 |
+
title="レンジング / 軌道位置 / 姿勢ビュー",
|
| 269 |
+
height=420,
|
| 270 |
+
margin=dict(l=10, r=10, t=45, b=10),
|
| 271 |
+
showlegend=False,
|
| 272 |
+
xaxis=dict(
|
| 273 |
+
visible=False,
|
| 274 |
+
range=[-650, 1250]
|
| 275 |
+
),
|
| 276 |
+
yaxis=dict(
|
| 277 |
+
visible=False,
|
| 278 |
+
range=[-650, 650],
|
| 279 |
+
scaleanchor="x",
|
| 280 |
+
scaleratio=1
|
| 281 |
+
),
|
| 282 |
+
)
|
| 283 |
+
return fig
|
| 284 |
+
|
| 285 |
+
def render_right_panel(target):
|
| 286 |
+
"""右半分の衛星可視化"""
|
| 287 |
+
s = st.session_state.sat_state
|
| 288 |
+
with target.container():
|
| 289 |
+
st.subheader("🛰️ Satellite Status")
|
| 290 |
+
|
| 291 |
+
c1, c2, c3 = st.columns(3)
|
| 292 |
+
c1.metric("高度", f"{s['altitude_km']} km")
|
| 293 |
+
c2.metric("速度", f"{s['speed_kms']} km/s")
|
| 294 |
+
c3.metric("バッテリー", f"{s['battery_pct']}%")
|
| 295 |
+
|
| 296 |
+
c4, c5, c6 = st.columns(3)
|
| 297 |
+
c4.metric("距離", f"{s['range_km']} km")
|
| 298 |
+
c5.metric("信号", f"{s['signal_db']} dB")
|
| 299 |
+
c6.metric("モード", s["mode"])
|
| 300 |
+
|
| 301 |
+
c7, c8, c9 = st.columns(3)
|
| 302 |
+
c7.metric("Yaw", f"{s['yaw_deg']}°")
|
| 303 |
+
c8.metric("Pitch", f"{s['pitch_deg']}°")
|
| 304 |
+
c9.metric("Roll", f"{s['roll_deg']}°")
|
| 305 |
+
|
| 306 |
+
st.plotly_chart(make_tracking_figure(), use_container_width=True)
|
| 307 |
+
|
| 308 |
+
health_df = pd.DataFrame(
|
| 309 |
+
{
|
| 310 |
+
"項目": ["Battery", "Signal", "Thermal"],
|
| 311 |
+
"値": [
|
| 312 |
+
s["battery_pct"],
|
| 313 |
+
s["signal_db"],
|
| 314 |
+
min(max(int((80 - abs(s["temp_c"] - 25) * 4)), 0), 100),
|
| 315 |
+
],
|
| 316 |
+
}
|
| 317 |
+
)
|
| 318 |
+
st.bar_chart(health_df.set_index("項目"))
|
| 319 |
+
|
| 320 |
+
st.caption(
|
| 321 |
+
f"Health: {s['health']} | Last event: {s['last_event']} | Updated: {datetime.now().strftime('%H:%M:%S')}"
|
| 322 |
+
)
|
| 323 |
+
|
| 324 |
+
# ----------------------------
|
| 325 |
+
# UI
|
| 326 |
+
# ----------------------------
|
| 327 |
+
st.title("🛰️ 衛星軌道保持AIシステム(PoC開発中)")
|
| 328 |
+
st.write("⚠️本アプリはデモであり、表示される内容は全てダミーです。")
|
| 329 |
+
st.write("左側で処理フロー、右側で衛星状態を可視化します。")
|
| 330 |
+
|
| 331 |
+
mission_text = st.text_area(
|
| 332 |
+
"ミッション指示",
|
| 333 |
+
value="衛星の軌道を保持してください。",
|
| 334 |
+
height=110,
|
| 335 |
+
)
|
| 336 |
+
|
| 337 |
+
run = st.button("ミッション開始", type="primary")
|
| 338 |
+
|
| 339 |
+
left_col, right_col = st.columns([1, 1], gap="large")
|
| 340 |
+
|
| 341 |
+
with left_col:
|
| 342 |
+
left_header = st.empty()
|
| 343 |
+
progress_box = st.empty()
|
| 344 |
+
status_box = st.empty()
|
| 345 |
+
log_box = st.empty()
|
| 346 |
+
result_box = st.empty()
|
| 347 |
+
|
| 348 |
+
with right_col:
|
| 349 |
+
sat_box = st.empty()
|
| 350 |
+
render_right_panel(sat_box)
|
| 351 |
+
|
| 352 |
+
# ----------------------------
|
| 353 |
+
# 実行
|
| 354 |
+
# ----------------------------
|
| 355 |
+
if run:
|
| 356 |
+
steps = [
|
| 357 |
+
{
|
| 358 |
+
"name": "制御計画/立案",
|
| 359 |
+
"desc": "条件を満たすパラメータ(スラスタセット/噴射秒数)を設定します。",
|
| 360 |
+
"action": lambda text: call_openai(
|
| 361 |
+
f"""
|
| 362 |
+
以下のミッション条件をもとに、軌道制御計画を立案してください。
|
| 363 |
+
- 使用するスラスタセット
|
| 364 |
+
- 想定される噴射秒数
|
| 365 |
+
- 計画時の前提条件
|
| 366 |
+
- 注意点
|
| 367 |
+
|
| 368 |
+
ミッション条件:
|
| 369 |
+
{text}
|
| 370 |
+
""".strip()
|
| 371 |
+
)
|
| 372 |
+
},
|
| 373 |
+
{
|
| 374 |
+
"name": "残推薬管理/確認",
|
| 375 |
+
"desc": "軌道制御に必要な消費推薬量を見積もります。",
|
| 376 |
+
"action": lambda text: call_openai(
|
| 377 |
+
f"""
|
| 378 |
+
以下の制御計画をもとに、残推薬管理の観点で評価してください。
|
| 379 |
+
- 想定される推薬消費量
|
| 380 |
+
- 残量への影響
|
| 381 |
+
- 運用上の注意点
|
| 382 |
+
- 地上局向けコメント
|
| 383 |
+
|
| 384 |
+
制御計画:
|
| 385 |
+
{text}
|
| 386 |
+
""".strip()
|
| 387 |
+
)
|
| 388 |
+
},
|
| 389 |
+
{
|
| 390 |
+
"name": "軌道決定",
|
| 391 |
+
"desc": "観測情報または制御結果をもとに衛星位置・軌道を決定します。",
|
| 392 |
+
"action": lambda text: call_openai(
|
| 393 |
+
f"""
|
| 394 |
+
以下の情報をもとに、軌道決定結果を日本語で簡潔にまとめてください。
|
| 395 |
+
- 現在の衛星位置・速度の整理
|
| 396 |
+
- 推定される軌道状態
|
| 397 |
+
- 判断根拠
|
| 398 |
+
- 不確かさや注意点
|
| 399 |
+
|
| 400 |
+
入力情報:
|
| 401 |
+
{text}
|
| 402 |
+
""".strip()
|
| 403 |
+
)
|
| 404 |
+
},
|
| 405 |
+
{
|
| 406 |
+
"name": "制御評価",
|
| 407 |
+
"desc": "軌道制御の結果と効率を評価します。",
|
| 408 |
+
"action": lambda text: call_openai(
|
| 409 |
+
f"""
|
| 410 |
+
以下の軌道決定結果をもとに、制御評価を行ってください。
|
| 411 |
+
- 制御結果の妥当性
|
| 412 |
+
- 目標達成度
|
| 413 |
+
- 効率の評価
|
| 414 |
+
- 改善点
|
| 415 |
+
- 地上局向けの簡潔な総括
|
| 416 |
+
|
| 417 |
+
軌道決定結果:
|
| 418 |
+
{text}
|
| 419 |
+
""".strip()
|
| 420 |
+
)
|
| 421 |
+
},
|
| 422 |
+
{
|
| 423 |
+
"name": "レポーティング",
|
| 424 |
+
"desc": "軌道制御の結果と効率をレポーティングします。",
|
| 425 |
+
"action": lambda text: call_openai(
|
| 426 |
+
f"""
|
| 427 |
+
以下の軌道決定結果をもとに、制御評価レポートを地上局向けに作成してください。
|
| 428 |
+
- 制御の成功可否
|
| 429 |
+
- 効率評価
|
| 430 |
+
- 推薬消費の妥当性
|
| 431 |
+
- 次回運用への示唆
|
| 432 |
+
|
| 433 |
+
軌道決定結果:
|
| 434 |
+
{text}
|
| 435 |
+
""".strip()
|
| 436 |
+
)
|
| 437 |
+
}
|
| 438 |
+
]
|
| 439 |
+
|
| 440 |
+
logs = []
|
| 441 |
+
outputs = {}
|
| 442 |
+
left_header.markdown("## 進行状況")
|
| 443 |
+
progress = progress_box.progress(0, text="待機中")
|
| 444 |
+
|
| 445 |
+
with status_box.container():
|
| 446 |
+
with st.status("処理中...", expanded=True) as status:
|
| 447 |
+
current_text = mission_text
|
| 448 |
+
|
| 449 |
+
for i, step in enumerate(steps):
|
| 450 |
+
pct = int(i / len(steps) * 100)
|
| 451 |
+
|
| 452 |
+
update_satellite_state(i)
|
| 453 |
+
render_right_panel(sat_box)
|
| 454 |
+
|
| 455 |
+
progress.progress(pct, text=f"Step {i+1}/{len(steps)}: {step['name']}")
|
| 456 |
+
logs.append(f"⏳ Step {i+1}: {step['name']} 開始")
|
| 457 |
+
log_box.markdown("\n\n".join(logs))
|
| 458 |
+
|
| 459 |
+
st.write(f"### Step {i+1}. {step['name']}")
|
| 460 |
+
st.write(step["desc"])
|
| 461 |
+
|
| 462 |
+
time.sleep(0.7)
|
| 463 |
+
result = step["action"](current_text)
|
| 464 |
+
outputs[step["name"]] = result
|
| 465 |
+
current_text = result
|
| 466 |
+
|
| 467 |
+
logs.append(f"✅ Step {i+1}: {step['name']} 完了")
|
| 468 |
+
log_box.markdown("\n\n".join(logs))
|
| 469 |
+
|
| 470 |
+
with st.expander(f"{step['name']} の出力", expanded=False):
|
| 471 |
+
st.write(result)
|
| 472 |
+
|
| 473 |
+
update_satellite_state(i + 1)
|
| 474 |
+
render_right_panel(sat_box)
|
| 475 |
+
time.sleep(0.5)
|
| 476 |
+
|
| 477 |
+
progress.progress(100, text="ミッション完了")
|
| 478 |
+
status.update(label="完了", state="complete", expanded=True)
|
| 479 |
|
| 480 |
+
with result_box.container():
|
| 481 |
+
st.markdown("## 最終レポート")
|
| 482 |
+
st.write(outputs.get("レポーティング", "出力なし"))
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
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|
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|
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|