TY  - BOOK
AU  - Bryson, Arthur E., Jr.
TI  - Control of spacecraft and aircraft
SN  - 069108722
CY  - Princeton
PB  - Princeton University Press
KW  - INGENIERIA AERONAUTICA
KW  - CONTROL AUTOMATICO DE AERONAVES
N1  - Apéndices a índice alfabético, al final del libro; Referencias bibliográficas p. 369376; Natural motions of rigid spacecraft :
Translational motions in space. Translstional motions in circular orbit. Rotational motions in space. rotational motions in circular orbit. Disturbances; Spacecraft sensors and attitude determination : 
Introduction. Infra-red, optical and radar sensors. Orbital gyrocompassing. Gyros. Inertial measurement units; Attitude control with thrusters :
Fast versus slow attitude control. Fast attitude control Using proportional thrusters. fast attitude control using on-off thrusters. Fast attitude contro using on-off thrusters; Attitude control with reaction wheels :
Fast control. Slowpitch control using gravity desaturation. Slow roll/yaw control using gravity desaturation; Attitude stabilization with spin :
Spinstabilization. Nutation damping. Dual spin. Offset axial trruster
; Attitude control with a gimbaled momentum Wheel :
Introduction. Fast control. Slow control using gravity desaturation; Attitude control during thrust maenuvers :
Using reation jets. Using a gimbaled engine. Using off-modulation or spin; Control of translational motions :
Fast control. Slow control in nearlu circular orbit; cross track. Slow control in circular orbit; in-track/radial; Flexibility and fuel slosh :
Introduction. Control synthesis using one vibration mode. Parasistic modes. control with fuel slosh. Robust compensator synthesis; Natural motions of rigid aircraft :
Equations of motion. Natural longitudinal motions. Natural lateral motions. Wind disturbances; Aircraft sensors :
Introduction. Vertical gyros. Directional gyros. Inertial measurement units. Baro-inertial altimeters; Control of longitudinal motions of aircraft :
Introduction. Steady-state control. Obsevability and controllability. Control of climb rate and airepeed. Control of altitude and airspeed. Glide-slope capture and hold. Flare; Control of lateral motions of aircraft :
Introduction. Steady bank angle and lateral specific force. Steady sideslip and yaw rate. Observability and controllability of lateral modes. Control of bank angle and sideforce. Control of track and sideforce; Control of helicopters near hover :
Introduction. Small deviations from steady hover. Steady-state control near hover. Control of velocity vector and yaw rate; Aeroelastic Systems :
Introduction. A simple system with a flutter mode. Flutter suppression for a simple system
ER  -