NDLI: A robust orbit design method for constant thrust collision avoidance maneuver

Content Provider	IEEE Xplore Digital Library
Author	Yongqiang Qi Yingmin Jia
Copyright Year	2014
Description	Author affiliation: Coll. of Sci., China Univ. of Min. & Technol. (CUMT), Beijing, China (Yongqiang Qi) \|\| Seventh Res. Div., Beihang Univ. (BUAA), Beijing, China (Yingmin Jia)
Abstract	In this paper, a robust constant thrust collision avoidance maneuver approach is proposed based on the relative motion dynamic model. First, the design problem is cast into a convex optimization problem by introducing a Lyapunov function subject to linear matrix inequalities. Next, the robust controllers satisfying the requirements can be designed by solving this optimization problem. Then, a new algorithm of constant thrust fitting is proposed through the impulse compensation and the fuel consumption under the theoretical continuous thrust and the actual constant thrust is calculated and compared by using the method proposed in this paper. At last, the proposed method has the advantage of saving fuel is proved and the actual constant thrust switch control laws are obtained through the isochronous interpolation method, an illustrative example is provided to show the effectiveness of the proposed control design method.
Starting Page	183
Ending Page	188
File Size	177691
Page Count	6
File Format	PDF
ISBN	9781479947003
e-ISBN	9781479946990
DOI	10.1109/CGNCC.2014.7007234
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-08-08
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Space vehicles Uncertainty Collision avoidance maneuver Switches Robust controller Linear matrix inequality Constant thrust Linear matrix inequalities Fuels Acceleration Collision avoidance Robots
Content Type	Text
Resource Type	Article

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