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CLC number: O232

On-line Access: 2020-07-10

Received: 2018-12-05

Revision Accepted: 2019-08-12

Crosschecked: 2020-03-06

Cited: 0

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Citations:  Bibtex RefMan EndNote GB/T7714


Li Xie


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Frontiers of Information Technology & Electronic Engineering  2020 Vol.21 No.7 P.1085-1107


Optimal two-impulse space interception with multiple constraints

Author(s):  Li Xie, Yi-qun Zhang, Jun-yan Xu

Affiliation(s):  State Key Laboratory of Alternate Electrical Power System with Renewable Energy Sources, School of Control and Computer Engineering, North China Electric Power University, Beijing 102206, China; more

Corresponding email(s):   lixie@ncepu.edu.cn, yiqunzhang@hotmail.com, junyan_Xu@sina.cn

Key Words:  Space interception problems, Variational method, Multiple constraints, Two-velocity impulses, Multi-point boundary value problems, Local optimal solutions, Dynamic slackness variable method

Li Xie, Yi-qun Zhang, Jun-yan Xu. Optimal two-impulse space interception with multiple constraints[J]. Frontiers of Information Technology & Electronic Engineering, 2020, 21(7): 1085-1107.

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A1 - Li Xie
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A1 - Jun-yan Xu
J0 - Frontiers of Information Technology & Electronic Engineering
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DOI - 10.1631/FITEE.1800763

We consider optimal two-impulse space interception problems with multiple constraints. The multiple constraints are imposed on the terminal position of a space interceptor, impulse and impact instants, and the component-wise magnitudes of velocity impulses. These optimization problems are formulated as multi-point boundary value problems and solved by the calculus of variations. Slackness variable methods are used to convert all inequality constraints into equality constraints so that the Lagrange multiplier method can be used. A new dynamic slackness variable method is presented. As a result, an indirect optimization method is developed. Subsequently, our method is used to solve the two-impulse space interception problems of free-flight ballistic missiles. A number of conclusions for local optimal solutions have been drawn based on highly accurate numerical solutions. Specifically, by numerical examples, we show that when time and velocity impulse constraints are imposed, optimal two-impulse solutions may occur; if two-impulse instants are free, then a two-impulse space interception problem with velocity impulse constraints may degenerate to a one-impulse case.





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