An operation of a spacecraft is controlled using an inner-loop control determining first control inputs for momentum exchange devices to control an orientation of the spacecraft and an outer-loop control determining second control inputs for thrusters of the spacecraft to concurrently control a pose of the spacecraft and a momentum stored by the momentum exchange devices of the spacecraft. The outer-loop control determines the second control inputs using a model of dynamics of the spacecraft including dynamics of the inner-loop control, such that the outer-loop control accounts for effects of actuation of the momentum exchange devices according to the first control inputs determined by the inner-loop control. The thrusters and the momentum exchange devices are controlled according to at least a portion of the first and the second control inputs.
METHOD AND SYSTEM FOR CONTROLLING OPERATION OF SPACECRAFT, SPACECRAFT
VERFAHREN UND SYSTEM ZUR STEUERUNG DES BETRIEBS EINES RAUMFAHRZEUGS, RAUMFAHRZEUG
PROCÉDÉ ET SYSTÈME PERMETTANT DE COMMANDER LE FONCTIONNEMENT D'UN ASTRONEF, ET ASTRONEF
2021-05-05
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
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