Attitude stabilization of spacecraft with two moving-mass via interconnection and damping assignment

Author

Yao, Yu ; Jiang, Yu

Author_Institution

Control & Simulation Center, Harbin Inst. of Technol., Harbin

fYear

2008

fDate

2-4 July 2008

Firstpage

5115

Lastpage

5118

Abstract

This paper deals with attitude control of spacecraft with two moving-mass. Two mass particles are constrained to move in different circular track fixed within the spacecraft, respectively. The dynamical model of the spacecraft is presented in a reduced dimensional Hamiltonian form. The Hamiltonian model is noncanonical and underactuated. We consider the application of interconnection and damping assignment to the problem of attitude stabilization of the underactuated spacecraft with two moving-mass.

Keywords

attitude control; space vehicles; stability; vehicle dynamics; attitude stabilization; circular track; damping assignment; interconnection; mass particles; moving mass; reduced dimensional Hamiltonian form; spacecraft; Attitude control; Control systems; Damping; Force control; Hydraulic actuators; Kinetic theory; Particle tracking; Space technology; Space vehicles; Weight control; Attitude Stabilization; Hamiltonian model; Interconnection and Damping Assignment; underactuated space-craft;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference, 2008. CCDC 2008. Chinese

Conference_Location

Yantai, Shandong

Print_ISBN

978-1-4244-1733-9

Electronic_ISBN

978-1-4244-1734-6

Type

conf

DOI

10.1109/CCDC.2008.4598304

Filename

4598304