Integrated Suboptimal Guidance and Control for Lunar Pinpoint Soft Landing
It proposed an integrated guidance and control method for lunar pinpoint soft landing to deal with the mismatch between the guidance system and control system in conventional separating design philosophy. The method is based on an improved ZEM/ZEV (zero-effort-miss/zero-effort-velocity) method and t...
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| Main Authors: | , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Control and Information Technology
2019-01-01
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| Series: | Kongzhi Yu Xinxi Jishu |
| Subjects: | |
| Online Access: | http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.100 |
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