An adaptive attitude control formulation under angular velocity constraints

Puneet Singla, Tarunraj Singh

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

6 Scopus citations

Abstract

An adaptive attitude control law which explicitly takes into account the constraints on individual angular velocity components has been developed for rigid body attitude control problem. Rigorous stability analysis is presented in the paper which guarantee the asymptotic stability of the controller. The performance of the control laws for stable, bounded tracking of attitude trajectories is evaluated. The essential ideas and results from computer simulations are presented to illustrate the performance of the controller developed in this paper.

Original languageEnglish (US)
Title of host publicationAIAA Guidance, Navigation and Control Conference and Exhibit
Publication statusPublished - Dec 1 2008
EventAIAA Guidance, Navigation and Control Conference and Exhibit - Honolulu, HI, United States
Duration: Aug 18 2008Aug 21 2008

Publication series

NameAIAA Guidance, Navigation and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation and Control Conference and Exhibit
CountryUnited States
CityHonolulu, HI
Period8/18/088/21/08

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All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering

Cite this

Singla, P., & Singh, T. (2008). An adaptive attitude control formulation under angular velocity constraints. In AIAA Guidance, Navigation and Control Conference and Exhibit [2008-6779] (AIAA Guidance, Navigation and Control Conference and Exhibit).