NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A Robust Control Approach for the Formation Flying of Multiple SpacecraftWe present a disturbance rejection mechanism for the formation flying of multiple spacecraft based on a robust control approach in terms of an H(sub infinity) control problem. The corresponding H(sub infinity) control problem is then solved numerically using linear matrix inequalities.
Document ID
20000056090
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Mesbahi, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Hadaegh, F. Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available