Control of spacecraft and aircraft Arthur E., Jr. Bryson

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