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Proceedings Paper

Missile autopilot design considering uncertainties in aerodynamics and actuator dynamics
Author(s): Yong D. Song; J. Hou; F. Fogson
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Paper 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.

Paper Details

Date Published: 7 July 2000
PDF: 12 pages
Proc. SPIE 4025, Acquisition, Tracking, and Pointing XIV, (7 July 2000); doi: 10.1117/12.391655
Show Author Affiliations
Yong D. Song, North Carolina A&T State Univ. (United States)
J. Hou, North Carolina A&T State Univ. (United States)
F. Fogson, North Carolina A&T State Univ. (United States)


Published in SPIE Proceedings Vol. 4025:
Acquisition, Tracking, and Pointing XIV
Michael K. Masten; Larry A. Stockum, Editor(s)

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