| 000 | 03322nam a22004217a 4500 | ||
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| 001 | NM002441 | ||
| 003 | AR-HaUTN | ||
| 005 | 20240930172227.0 | ||
| 007 | ta | ||
| 008 | 51120sc. 1 ||||||||||||||000 | spa|| | ||
| 020 | _a069108722 | ||
| 040 |
_aAR-HaUTN _cAR-HaUTN |
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| 100 |
_aBryson, Arthur E., Jr. _93056 |
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| 245 |
_aControl of spacecraft and aircraft _cArthur E., Jr. Bryson |
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| 250 | _a[1st?] ed. | ||
| 260 |
_aPrinceton _bPrinceton University Press |
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| 300 |
_axxiii, 378 p. _bgráficos |
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| 500 | _aApéndices a índice alfabético, al final del libro | ||
| 504 | _aReferencias bibliográficas p. 369376 | ||
| 505 | _tNatural motions of rigid spacecraft : Translational motions in space. Translstional motions in circular orbit. Rotational motions in space. rotational motions in circular orbit. Disturbances | ||
| 505 | _tSpacecraft sensors and attitude determination : Introduction. Infra-red, optical and radar sensors. Orbital gyrocompassing. Gyros. Inertial measurement units | ||
| 505 | _tAttitude 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 | ||
| 505 | _tAttitude control with reaction wheels : Fast control. Slowpitch control using gravity desaturation. Slow roll/yaw control using gravity desaturation | ||
| 505 | _tAttitude stabilization with spin : Spinstabilization. Nutation damping. Dual spin. Offset axial trruster | ||
| 505 | _tAttitude control with a gimbaled momentum Wheel : Introduction. Fast control. Slow control using gravity desaturation | ||
| 505 | _tAttitude control during thrust maenuvers : Using reation jets. Using a gimbaled engine. Using off-modulation or spin | ||
| 505 | _tControl of translational motions : Fast control. Slow control in nearlu circular orbit; cross track. Slow control in circular orbit; in-track/radial | ||
| 505 | _tFlexibility and fuel slosh : Introduction. Control synthesis using one vibration mode. Parasistic modes. control with fuel slosh. Robust compensator synthesis | ||
| 505 | _tNatural motions of rigid aircraft : Equations of motion. Natural longitudinal motions. Natural lateral motions. Wind disturbances | ||
| 505 | _tAircraft sensors : Introduction. Vertical gyros. Directional gyros. Inertial measurement units. Baro-inertial altimeters | ||
| 505 | _tControl 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 | ||
| 505 | _tControl 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 | ||
| 505 | _tControl of helicopters near hover : Introduction. Small deviations from steady hover. Steady-state control near hover. Control of velocity vector and yaw rate | ||
| 505 | _tAeroelastic Systems : Introduction. A simple system with a flutter mode. Flutter suppression for a simple system | ||
| 653 | _aINGENIERIA AERONAUTICA | ||
| 653 | _aCONTROL AUTOMATICO DE AERONAVES | ||
| 942 |
_cBK _2udc |
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| 999 |
_c2441 _d2441 |
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