Modern Spacecraft Dynamics and Control |
Contents
INTRODUCTION | 1 |
General Equation 13 Motion of the Earths | 17 |
Central Force Motion 29 Keplers Time Equa | 37 |
Copyright | |
27 other sections not shown
Other editions - View all
Common terms and phrases
acceleration angle angular momentum applied approach associated assumed attitude attraction axes axis becomes body calculated center of mass Chapter circular components Consider constant coordinates corresponding damping defined described determine developed device direction dissipation earth effects ellipse energy equation error example expression Figure final flight force frame function gimbal given gives gyro illustrated impulse inertia initial integration interest km/s leads limit locus magnitude maneuver mass method motion moving normal Note nutation obtained orbit orientation parameters path period permits perturbing pitch plane poles position possible precession presented principal problem reference relative represent respect result roll rotation satellite satisfy selected sensor shown simple situation solution space spacecraft specified spin stability step technique torque transfer transformation vector vehicle velocity wheel yields zero