Research on Minimum Time Interception Problem with a Tangent Impulse under Relative Motion Models

The minimum time interception problem with a tangent impulse whose direction is the same as the satellite’s velocity direction is studied based on the relative motion equations of elliptical orbits by the combination of analytical, numerical, and optimization methods. Firstly, the feasible domain of...

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Bibliographic Details
Main Authors: Wenzhe Ding, Xinhong Li, Hong Yang
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/6827982
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