Relative State and Inertia Estimation of Unknown Tumbling Spacecraft by Stereo Vision

Engineering

• Relative Position 100%
• Feature Point 100%
• Angular Velocity ω 100%
• Stereovision 100%
• Optimization Method 50%
• Square Method 50%
• Least Square 50%
• Physical Constraint 50%
• Angular Momentum 50%
• Motion Model 50%
• Momentum Conservation 50%
• Linear Velocity 50%