Some control strategies for a high-angle-of-attack missile autopilot

E Devaud, H Siguerdidjane, S Font - Control Engineering Practice, 2000 - Elsevier
Recent interest in high maneuverability and stealth in missiles has triggered new
investigations in estimating the potential and applicability of recent theoretical control …

Nonlinear missile autopilot design based on angle of attack normal form

H Siguerdidjane, E Devaud - European Journal of Control, 2000 - Elsevier
A nonlinear controllalv is proposed to make the normal acceleration of a high angle of attack
missile track some desired trajectories. The angle of attack canonicalform is first derived …