An attitude control system and method operative with a thruster controls the attitude of a vehicle carrying the thruster, wherein the thruster has a valve enabling the formation of pulses of expelled gas from a source of compressed gas. Data of the attitude of the vehicle is gathered, wherein the vehicle is located within a force field tending to orient the vehicle in a first attitude different from a desired attitude. The attitude data is evaluated to determine a pattern of values of attitude of the vehicle in response to the gas pulses of the thruster and in response to the force field. The system and the method maintain the attitude within a predetermined band of values of attitude which includes the desired attitude. Computation circuitry establishes an optimal duration of each of the gas pulses based on the pattern of values of attitude, the optimal duration providing for a minimal number of opening and closure operations of the valve. The thruster is operated to provide gas pulses having the optimal duration.
Adaptive mass expulsion attitude control system
2001-03-20
Sonstige
Keine Angabe
Englisch
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model
Springer Verlag | 2013
|Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model
Online Contents | 2013
|