TY - GEN

T1 - UAV guidance system with combined adaptive autopilot

AU - Andrievsky, Boris R.

AU - Fradkov, Alexander L.

PY - 2003

Y1 - 2003

N2 - Combined adaptive control law for an autopilot of the UAV homing guidance system is proposed. The adaptation algorithm provides prescribed attitude motion dynamics for different flight conditions. Simulation results verify efficiency of the combined adaptive controller in the case of significant uncertainty of the UAV parameters and time-dependence of the guidance loop.

AB - Combined adaptive control law for an autopilot of the UAV homing guidance system is proposed. The adaptation algorithm provides prescribed attitude motion dynamics for different flight conditions. Simulation results verify efficiency of the combined adaptive controller in the case of significant uncertainty of the UAV parameters and time-dependence of the guidance loop.

KW - Adaptive control

KW - Identification

KW - Sliding mode controller

KW - UAV Guidance

UR - http://www.scopus.com/inward/record.url?scp=1542643500&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:1542643500

SN - 0889863555

T3 - Proceedings of the IASTED International Conference on Intelligent Systems and Control

SP - 91

EP - 93

BT - Proceedings of the IASTED International Conference on Intelligent Systems and Control

A2 - Hamza, M.H.

A2 - Hamza, M.H.

T2 - Proceedings of the IASTED International Conference on Intelligent Systems and Control

Y2 - 25 June 2003 through 27 June 2003

ER -