Guidance, navigation and control for autonomous R-bar proximity operations for geostationary satellites

Engineering

• Attitude Control 100%
• Geostationary Satellite 100%
• Simulation Result 50%
• Flight Time 50%
• Sliding Mode 50%
• Extended Kalman Filter 50%
• Control Law 50%
• Control Algorithm 50%
• Sensor Measurement 50%
• Angular Velocity ω 50%
• Optical Axis 50%
• Inertial Frame 50%
• Orbit Control 50%
• Fixed Reference Frame 50%

Earth and Planetary Sciences

• Geostationary Satellite 100%
• Line of Sight 100%
• Kalman Filter 50%
• Attitude Control 50%
• Flight Time 50%