Output feedback control for spacecraft with coupled translation and attitude dynamics

Haizhou Pan, Hong Wong, Vikram Kapila

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

Abstract

In this paper, we address a tracking control problem for a spacecraft with coupled translation and attitude motion, in the absence of translation and angular velocity measurements. We begin by describing the mutually coupled translation and attitude dynamics of the spacecraft. Next, a suitable high-pass filter is employed to estimate the spacecraft translation and angular velocities using measurements of its translational position and attitude orientation. Using a Lyapunov framework, a nonlinear output feedback control law is designed that ensures the semi-global asymptotic convergence of the spacecraft translation and attitude position tracking errors, despite the lack of translation and angular velocity feedback.

Original languageEnglish (US)
Title of host publicationProceedings of the IEEE Conference on Decision and Control
Pages4453-4458
Number of pages6
Volume4
StatePublished - 2004
Event2004 43rd IEEE Conference on Decision and Control (CDC) - Nassau, Bahamas
Duration: Dec 14 2004Dec 17 2004

Other

Other2004 43rd IEEE Conference on Decision and Control (CDC)
CountryBahamas
CityNassau
Period12/14/0412/17/04

Fingerprint

Feedback control
Spacecraft
Angular velocity
Angle measurement
Velocity measurement
High pass filters
Feedback

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Safety, Risk, Reliability and Quality
  • Chemical Health and Safety

Cite this

Pan, H., Wong, H., & Kapila, V. (2004). Output feedback control for spacecraft with coupled translation and attitude dynamics. In Proceedings of the IEEE Conference on Decision and Control (Vol. 4, pp. 4453-4458). [FrA10.1]

Output feedback control for spacecraft with coupled translation and attitude dynamics. / Pan, Haizhou; Wong, Hong; Kapila, Vikram.

Proceedings of the IEEE Conference on Decision and Control. Vol. 4 2004. p. 4453-4458 FrA10.1.

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

Pan, H, Wong, H & Kapila, V 2004, Output feedback control for spacecraft with coupled translation and attitude dynamics. in Proceedings of the IEEE Conference on Decision and Control. vol. 4, FrA10.1, pp. 4453-4458, 2004 43rd IEEE Conference on Decision and Control (CDC), Nassau, Bahamas, 12/14/04.
Pan H, Wong H, Kapila V. Output feedback control for spacecraft with coupled translation and attitude dynamics. In Proceedings of the IEEE Conference on Decision and Control. Vol. 4. 2004. p. 4453-4458. FrA10.1
Pan, Haizhou ; Wong, Hong ; Kapila, Vikram. / Output feedback control for spacecraft with coupled translation and attitude dynamics. Proceedings of the IEEE Conference on Decision and Control. Vol. 4 2004. pp. 4453-4458
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