Tracking control for angular-rate-sensorless vertical take-off and landing aircraft in the presence of angular-position measurement delay
作者： B. Zhu , X. Wang , K.-Y. Cai
DOI: 10.1049/IET-CTA.2009.0139
关键词: Angular displacement 、 Attitude control 、 Control engineering 、 Backstepping 、 Angular velocity 、 Control theory 、 Control theory 、 Observer (quantum physics) 、 Differentiator 、 Engineering 、 Tracking (particle physics)
摘要: In this study, the authors address non-linear tracking problem of a roll-rate-sensorless vertical take-off and landing aircraft in presence roll-angle measurement delay. By using first-order Pade approximation signal delayed roll angle, develop an extended attitude observer controller based on observer, two global coordinate transformations extension backstepping technique. Moreover, finite-time-convergent differentiator is introduced to simplify computation one control signals. The resulting approximate practicable for actual implementation. Numerical simulations are performed show effectiveness controller.
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