7 July 2000 Missile autopilot design considering uncertainties in aerodynamics and actuator dynamics
Author Affiliations +
Abstract
This work presents a method for missile autopilot design in the presence of actuator and uncertain dynamics. Nonlinear control algorithms are derived based on both missile aerodynamics and actuator dynamics. To account for system nonlinearities and uncertainties due to varying flight conditions, a memory-based compensation unit is developed and integrated into the strategy. Simulation on EMRAAT missile validates the effectiveness of the proposed control method.
© (2000) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Yong D. Song, Yong D. Song, J. Hou, J. Hou, F. Fogson, F. Fogson, } "Missile autopilot design considering uncertainties in aerodynamics and actuator dynamics", Proc. SPIE 4025, Acquisition, Tracking, and Pointing XIV, (7 July 2000); doi: 10.1117/12.391655; https://doi.org/10.1117/12.391655
PROCEEDINGS
12 PAGES


SHARE
Back to Top