Fault Tolerant Tracking Control for a Team of Non-Minimum Phase VTOL Aircrafts Based on Virtual Leader Structure
Author:
Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-662-48386-2_25
Reference13 articles.
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3. Wang XH (2013) Takeoff/landing control based on acceleration measurements for VTOL aircraft [J]. J Franklin Inst 350(10):3045–3063
4. Al-Hiddabi SA, McClamroch NH (1998) Output tracking for nonlinear non-minimum phase VTOL aircraft [C]. In: Proceedings of the 37th IEEE conference on decision and control, vol 4, pp 4573–4578
5. Cai KY, Liu JK, Wang XH (2009) Tracking control for a velocity sensor-less vertical take-off and landing aircraft with delayed outputs. Automatica 45(12):2876–2882
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