Fast Attitude Maneuvers for NASA’s Lunar Reconnaissance Orbiter: Practical Flight Application of Attitude Guidance using Birkhoff Pseudospectral Theory and Hamiltonian Programming
IEEE Control Systems Magazine(2024)
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Lunar Reconnaissance Orbiter,Attitude Maneuver,Positive Control,Optimization Problem,Optimal Control,Nonlinear Programming,Synthetic Aperture Radar,Closed-loop Control,Trajectory Optimization,Angular Speed,Science Team,Spaceflight,Scientific Observations,Cold Trap,Space Robot,Subsurface Temperature,Science Missions,Mission Performance,Thermal Constraints,Trajectory Optimization Problem,Angular Acceleration,Body-fixed Frame,KKT Conditions,Shortest Path,High-fidelity Simulation,Rigid Body,Technological Constraints,Solar Array,Pseudospectral Method,L1-norm
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