TY - GEN
T1 - Adaptive control of a rigid body vehicle on exponential coordinates with guaranteed performance
AU - Arabi, Ehsan
AU - Sarsilmaz, Selahattin Burak
AU - Yucelen, Tansel
AU - Maadani, Mohammad
AU - Butcher, Eric A.
AU - Nazari, Morad
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018/1/1
Y1 - 2018/1/1
N2 - Adaptive control systems are widely used for compensating the effect of disturbances, system uncertainties, unmodeled dynamics, and changes in systemdynamics. In this paper, the problemof controlling an uncertain rigid body vehicle is investigated for tracking a desired trajectory, where the relative configuration is described in terms of exponential coordinates on the Lie group of rigid body motions. First, one of the existing nominal controllers, which provides coupled translational and rotational maneuvers, is augmented with an adaptive controller to suppress the effects of systemuncertainties. Second, in order to achieve a prescribed user-defined performance guarantee, nominal controller is augmented with set-theoretic adaptive controller to enforce the systemstate trajectory to evolve inside a-priori user-defined compact set. Finally, the efficacy of the presented theoretical results are demonstrated through an illustrative numerical example.
AB - Adaptive control systems are widely used for compensating the effect of disturbances, system uncertainties, unmodeled dynamics, and changes in systemdynamics. In this paper, the problemof controlling an uncertain rigid body vehicle is investigated for tracking a desired trajectory, where the relative configuration is described in terms of exponential coordinates on the Lie group of rigid body motions. First, one of the existing nominal controllers, which provides coupled translational and rotational maneuvers, is augmented with an adaptive controller to suppress the effects of systemuncertainties. Second, in order to achieve a prescribed user-defined performance guarantee, nominal controller is augmented with set-theoretic adaptive controller to enforce the systemstate trajectory to evolve inside a-priori user-defined compact set. Finally, the efficacy of the presented theoretical results are demonstrated through an illustrative numerical example.
UR - http://www.scopus.com/inward/record.url?scp=85141603146&partnerID=8YFLogxK
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U2 - 10.2514/6.2018-1106
DO - 10.2514/6.2018-1106
M3 - Conference contribution
AN - SCOPUS:85141603146
SN - 9781624105265
T3 - AIAA Guidance, Navigation, and Control Conference, 2018
BT - AIAA Guidance, Navigation, and Control
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -