Wave-Based Attitude Control of Spacecraft with Fuel Sloshing Dynamics

Archive of Mechanical Engineering

Thompson Joseph William¹  O’Connor William¹ 

[1] School of Mechanical and Materials Engineering, University College Dublin, Belfield, Dublin 4, Ireland;

关键词: spacecraft dynamic;    attitude control;    flexible systems;    sloshing;    mechanical Waves;   

DOI  :  10.1515/meceng-2016-0015

来源: DOAJ

【 摘 要 】

Wave-Based Control has been previously applied successfully to simple under-actuated flexible mechanical systems. Spacecraft and rockets with structural flexibility and sloshing are examples of such systems but have added difficulties due to non-uniform structure, external disturbing forces and non-ideal actuators and sensors. The aim of this paper is to extend the application of WBC to spacecraft systems, to compare the performance of WBC to other popular controllers and to carry out experimental validation of the designed control laws. A mathematical model is developed for an upper stage accelerating rocket moving in a single plane. Fuel sloshing is represented by an equivalent mechanical pendulum model. A wave-based controller is designed for the upper stage AVUM of the European launcher Vega. In numerical simulations the controller successfully suppresses the sloshing motion. A major advantage of the strategy is that no measurement of the pendulum states (sloshing motion) is required.

【 授权许可】

Unknown