Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description
For the obstacle avoidance and formation maintenance issues of spacecraft formation, a control method with prescribed performance is proposed. Firstly, an error description system based on SE (3) is established. Secondly, to simplify the control system, collision avoidance, formation control of lead...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2025-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/ijae/8765666 |
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