Spaceflight Mechanics 1996: Proceedings of the AAS/AIAA Spaceflight Mechanics Conference Held February 12-15, 1996, Austin, Texas, Part 2G. Edward Powell |
Contents
A Fast onBoard Autonomous Attitude Determination System Based on | 893 |
FOREWORD vii | 903 |
Nonlinear Instabilities in a DualSpin Spacecraft With an Axial Nutational | 905 |
Copyright | |
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AAS Microfiche Series AAS/AIAA acceleration accuracy algorithm altimeter amplitude analysis angle angular velocity antenna arcs Astrodynamics attitude control axis coefficients components computed configuration constant coordinates covariance crossover cycle debris cloud dynamics estimation external torque Figure flight frequency GEOSAT geosynchronous gravity Hard Cover inertial initial integration ISBN Kalman filter Koreasat libration linear Lyapunov function magnitude maneuver mass matrix measurements method Microfiche Microfiche Suppl mission model error momentum navigation noise obtained optimal orbit determination orbit error orbital frame parameters payload performance period perturbation phase position predicted problem propulsion pseudorange radial reference relative repetitive control residual rotation satellite semi-major axis sensors shown Shuttle simulation Soft Cover solar solar sail solution Space spacecraft startracker station subsystem Table technique tether Texas thrust thruster TOPEX/POSEIDON torque trajectory true anomaly values vector vehicle vibration zero