论文信息 - Orbital Experiments of Linearly Interpolated Gain Scheduling Attitude Controller Using ETS-VIII Spacecraft

Orbital Experiments of Linearly Interpolated Gain Scheduling Attitude Controller Using ETS-VIII Spacecraft

Abstract This paper describes orbital attitude control experiments carried out on the ETS (Engineering Test Satellite)-VIII in June 2009. These experiments aim to develop a technical basis for the orbital control of a class of future large flexible spacecraft. Several novel robust control laws were tested, including a μ-synthesis based control law, a DVDFB (Direct Velocity and Displacement FeedBack) control law and a linearly interpolated gain scheduling law. Among them, this paper focuses on the gain scheduling law. Experimental results of this control law are presented to show its high control performance and lower computational burden compared with other control laws.

[1] Takashi Kida,et al. Robust Attitude Control Using Mu-Synthesis for the Large Flexible Satellite ETS-VIII , 2009 .

[2] Jonathan P. How,et al. Robust control design and implementation on the Middeck Active Control Experiment , 1994 .

[3] M. Balas. Active control of flexible systems , 1978 .

[4] Takashi Kida,et al. GAIN SCHEDULING CONTROLLER DESIGN FOR ENGINEERING TEST SATELLITE-VIII , 2007 .

[5] Angelia P. Bukley,et al. Hubble Space Telescope Pointing Control System Design Improvement Study Results , 1995 .

[6] Takashi Kida,et al. On-Orbit Robust Control Experiment of Flexible Spacecraft ETS-VI , 1997 .

[7] Takashi Kida,et al. Design and Implementation of Robust Symmetric Attitude Controller for ETS-VIII Spacecraft , 2008 .