An Interpolated Model Recovery Anti-Windup for a Canard-Guided Projectile Subject to Uncertainties

This paper presents an autopilot design for a dual-spin guided projectile subject to aerodynamic uncertainties and actuator saturations. The proposed design consists of a gain-scheduled baseline controller together with an interpolated dynamic anti-windup compensator based on model recovery. Evaluat...

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Veröffentlicht in:	2021 European Control Conference (ECC) S. 1693 - 1698
Hauptverfasser:	Thai, Sovanna, Roos, Clement, Biannic, Jean-Marc, Theodoulis, Spilios
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	EUCA 29.06.2021
Schlagworte:	Aerodynamics anti-windup Autopilot autopilot design gain scheduling guided projectiles Monte Carlo methods Projectiles Robustness robustness analysis Sensitivity Uncertainty
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Zusammenfassung:	This paper presents an autopilot design for a dual-spin guided projectile subject to aerodynamic uncertainties and actuator saturations. The proposed design consists of a gain-scheduled baseline controller together with an interpolated dynamic anti-windup compensator based on model recovery. Evaluation of the closed-loop is done through IQC-based analysis at an operating point, and through Monte Carlo simulations. Both assessments show that the addition of an anti-windup compensator can drastically improve the behaviour of the system in degraded flight conditions.
DOI:	10.23919/ECC54610.2021.9655059