Robust adaptive control of formationkeeping for a pair of satellites

Zhi Wang, Farshad Khorrami, Walter Grossman

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Two robust adaptive control schemes (state-feedback and output-feedback) for formationkeeping of a pair of satellites are proposed in this paper. In contrast to most existing results, both control schemes are based on the nonlinear model directly, not on the simplified linearized model. In addition, the uncertainties and disturbances in the system such as the effects due to solar pressure, noncentral gravitational field, air drag, and etc. are all considered. The objective of the control design is to force the relative position between two satellites track a given reference signal while maintaining the desired Keplerian trajectory (in this case circular) for master satellite The results of this paper may be easily generalized to formationkeeping of a number of satellites.

Original languageEnglish (US)
Title of host publicationProceedings of the American Control Conference
PublisherIEEE
Pages834-838
Number of pages5
Volume2
StatePublished - 2000
Event2000 American Control Conference - Chicago, IL, USA
Duration: Jun 28 2000Jun 30 2000

Other

Other2000 American Control Conference
CityChicago, IL, USA
Period6/28/006/30/00

Fingerprint

Satellites
Hydrostatic pressure
State feedback
Drag
Trajectories
Feedback
Air
Uncertainty

ASJC Scopus subject areas

  • Control and Systems Engineering

Cite this

Wang, Z., Khorrami, F., & Grossman, W. (2000). Robust adaptive control of formationkeeping for a pair of satellites. In Proceedings of the American Control Conference (Vol. 2, pp. 834-838). IEEE.

Robust adaptive control of formationkeeping for a pair of satellites. / Wang, Zhi; Khorrami, Farshad; Grossman, Walter.

Proceedings of the American Control Conference. Vol. 2 IEEE, 2000. p. 834-838.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Wang, Z, Khorrami, F & Grossman, W 2000, Robust adaptive control of formationkeeping for a pair of satellites. in Proceedings of the American Control Conference. vol. 2, IEEE, pp. 834-838, 2000 American Control Conference, Chicago, IL, USA, 6/28/00.
Wang Z, Khorrami F, Grossman W. Robust adaptive control of formationkeeping for a pair of satellites. In Proceedings of the American Control Conference. Vol. 2. IEEE. 2000. p. 834-838
Wang, Zhi ; Khorrami, Farshad ; Grossman, Walter. / Robust adaptive control of formationkeeping for a pair of satellites. Proceedings of the American Control Conference. Vol. 2 IEEE, 2000. pp. 834-838
@inproceedings{10bbdd1f35d64be6bff4a83659e2009a,
title = "Robust adaptive control of formationkeeping for a pair of satellites",
abstract = "Two robust adaptive control schemes (state-feedback and output-feedback) for formationkeeping of a pair of satellites are proposed in this paper. In contrast to most existing results, both control schemes are based on the nonlinear model directly, not on the simplified linearized model. In addition, the uncertainties and disturbances in the system such as the effects due to solar pressure, noncentral gravitational field, air drag, and etc. are all considered. The objective of the control design is to force the relative position between two satellites track a given reference signal while maintaining the desired Keplerian trajectory (in this case circular) for master satellite The results of this paper may be easily generalized to formationkeeping of a number of satellites.",
author = "Zhi Wang and Farshad Khorrami and Walter Grossman",
year = "2000",
language = "English (US)",
volume = "2",
pages = "834--838",
booktitle = "Proceedings of the American Control Conference",
publisher = "IEEE",

}

TY - GEN

T1 - Robust adaptive control of formationkeeping for a pair of satellites

AU - Wang, Zhi

AU - Khorrami, Farshad

AU - Grossman, Walter

PY - 2000

Y1 - 2000

N2 - Two robust adaptive control schemes (state-feedback and output-feedback) for formationkeeping of a pair of satellites are proposed in this paper. In contrast to most existing results, both control schemes are based on the nonlinear model directly, not on the simplified linearized model. In addition, the uncertainties and disturbances in the system such as the effects due to solar pressure, noncentral gravitational field, air drag, and etc. are all considered. The objective of the control design is to force the relative position between two satellites track a given reference signal while maintaining the desired Keplerian trajectory (in this case circular) for master satellite The results of this paper may be easily generalized to formationkeeping of a number of satellites.

AB - Two robust adaptive control schemes (state-feedback and output-feedback) for formationkeeping of a pair of satellites are proposed in this paper. In contrast to most existing results, both control schemes are based on the nonlinear model directly, not on the simplified linearized model. In addition, the uncertainties and disturbances in the system such as the effects due to solar pressure, noncentral gravitational field, air drag, and etc. are all considered. The objective of the control design is to force the relative position between two satellites track a given reference signal while maintaining the desired Keplerian trajectory (in this case circular) for master satellite The results of this paper may be easily generalized to formationkeeping of a number of satellites.

UR - http://www.scopus.com/inward/record.url?scp=0034542499&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0034542499&partnerID=8YFLogxK

M3 - Conference contribution

VL - 2

SP - 834

EP - 838

BT - Proceedings of the American Control Conference

PB - IEEE

ER -