Yan, Xinggang (1993) Trajectory of spacecraft and its escape criteria under radial continuous thrust (??????????????????). Journal of Harbin University of Science and technology, (4). pp. 98-105. ISSN 1007-2683. (The full text of this publication is not currently available from this repository. You may be able to access a copy if URLs are provided) (KAR id:51849)
| The full text of this publication is not currently available from this repository. You may be able to access a copy if URLs are provided. | |
| Official URL: http://lib.cqvip.com/qk/93729X/199304/ |
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| Item Type: | Article |
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| Additional information: | This paper is in Chinese version |
| Subjects: | T Technology > TJ Mechanical engineering and machinery > Control engineering |
| Institutional Unit: | Schools > School of Engineering, Mathematics and Physics > Engineering |
| Former Institutional Unit: |
Divisions > Division of Computing, Engineering and Mathematical Sciences > School of Engineering and Digital Arts
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| Depositing User: | Xinggang Yan |
| Date Deposited: | 14 Nov 2015 13:11 UTC |
| Last Modified: | 20 May 2025 10:40 UTC |
| Resource URI: | https://kar.kent.ac.uk/id/eprint/51849 (The current URI for this page, for reference purposes) |
University of Kent Author Information
Yan, Xinggang.
| Creator's ORCID: |
 https://orcid.org/0000-0003-2217-8398
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