Abstract
In this paper, variable thrust angle (VTA) constant thrust collision avoidance maneuver is studied. For in-plane motion, robust controllers satisfying the requirements can be designed by solving this optimization problem. For out-plane motion, a new algorithm of constant thrust fitting is proposed through impulse compensation and fuel consumption under theoretical continuous thrust and the actual constant thrust is calculated. Finally, illustrative example is provided to show the effectiveness of the proposed control design method.
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Acknowledgments
This work was supported by the NSFC 61304088 and 2013QNA37.
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© 2015 Springer-Verlag Berlin Heidelberg
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Qi, Y., Ma, Y. (2015). Variable Thrust Angle Constant Thrust Collision Avoidance Maneuver. In: Deng, Z., Li, H. (eds) Proceedings of the 2015 Chinese Intelligent Automation Conference. Lecture Notes in Electrical Engineering, vol 337. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-46463-2_1
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DOI: https://doi.org/10.1007/978-3-662-46463-2_1
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Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-662-46462-5
Online ISBN: 978-3-662-46463-2
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