A robust control approach for the formation flying of multiple spacecraft

Author

Mesbahi, M. ; Hadaegh, F.Y.

Author_Institution

Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA

fYear

1999

fDate

Aug. 31 1999-Sept. 3 1999

Firstpage

2933

Lastpage

2938

Abstract

We present a disturbance rejection mechanism for the formation flying of multiple spacecraft based on a robust control approach in terms of an H_∞ control problem. The corresponding H_∞ control problem is then solved numerically using linear matrix inequalities.

Keywords

H^∞ control; active disturbance rejection control; linear matrix inequalities; position control; space vehicles; H_∞ control problem; LMI; disturbance rejection mechanism; linear matrix inequalities; robust control; spacecraft formation flying; Aerodynamics; Angular velocity; Force; Linear matrix inequalities; Space vehicles; State feedback; Torque; Formation flying; disturbance rejection; linear matrix inequality; robust control;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (ECC), 1999 European

Conference_Location

Karlsruhe

Print_ISBN

978-3-9524173-5-5

Type

conf

Filename

7099774

Link To Document

https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=706829