Advances in the Astronautical Sciences
George W. Morganthaler
American Astronautical Society, 1987 - Science - 1777 pages
Vols. 1- are the Proceedings of the American Astronautical Society's annual and West Coast meetings and Symposia of the Society.
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A ThreeStage Approach to Optimal LowThrust EarthMoon
FOREWORD Robert H Jacobs
ATTITUDE DETERMINATION AND CONTROL 1
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AIAA algorithm altimeter analytical angle angular momentum angular velocity applied approximate ascending node Astrodynamics attitude axis chaos diagrams components computed control law convergence coordinate defined derived determined differential equations disturbance dynamics eccentricity elements energy ephemeris equations of motion error Euler angles Euler's equations feedback Figure first-order flexible space formulation frame frequency function GEOSAT given gravity Hansen coefficients initial conditions input integration interval Journal of Guidance laser learning control linear Lyapunov exponents maneuver manipulator mass center matrix method mode neural nonlinear numerical obtained optimal orbit order system output paper perigee perturbations pitch platform polynomials position problem reorientation repetitive control rigid body robot rotation satellite semi-major axis shown simulation slew solar solution Space Station spacecraft stability structure switching thrust thrusters time-optimal TOPEX/POSEIDON torque tracking trajectory true anomaly two-body two-body problem values variables vector vibration zero