πŸŒ™ LUNAR LANDER

Control Demonstration System
samilkorkmaz/pidLunarLander
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MANUAL
Environment
Gravity (m/sΒ²) 1.62
Max Thrust (N/kg) 3.50
Initial Altitude (m) 500
Thrust Dynamics
First-Order Lag ON
K β€” Steady-state gain 1.00
Ο„ β€” Time constant (s) 0.5
Commanded β–‘ vs Realized β–ˆ
Control Mode
Thrust Control
0%
β–² Increase
β–Ό Decrease
SPACE Cut
PID Internals
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Thrust History
Commanded
Realized
Thrust Telemetry
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Telemetry
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Safe Landing Criteria
≀ 5 m/s
≀ 4 m
Data Export
0 frames recorded