Please use this identifier to cite or link to this item: https://doi.org/10.1109/ICCA.2011.6137973
Title: Minimum time control of helicopter UAVs using computational dynamic optimization
Authors: Tang, K.
Wang, B. 
Kang, W.
Chen, B. 
Issue Date: 2011
Source: Tang, K.,Wang, B.,Kang, W.,Chen, B. (2011). Minimum time control of helicopter UAVs using computational dynamic optimization. IEEE International Conference on Control and Automation, ICCA : 848-852. ScholarBank@NUS Repository. https://doi.org/10.1109/ICCA.2011.6137973
Abstract: This paper focuses on the problem of minimum time trajectory planning for helicopter UAVs. It is formulated as a nonlinear optimal control subject to the dynamics and limitations of helicopter UAVs. The dynamical system is defined by a set of fifteen states nonlinear differential equations developed for HeLion, a UAV helicopter constructed in National University of Singapore (NUS). The problem is then solved numerically using pseudospectral method for dynamic optimization. The results show that minimum time trajectories are highly nonlinear that require complicated maneuvering. © 2011 IEEE.
Source Title: IEEE International Conference on Control and Automation, ICCA
URI: http://scholarbank.nus.edu.sg/handle/10635/70949
ISBN: 9781457714757
ISSN: 19483449
DOI: 10.1109/ICCA.2011.6137973
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