Constrained Control for Spacecraft Rendezvous System With Multiple Input Delays
This paper studies the stability of the spacecraft rendezvous system with asymmetric input saturation and multiple input delay based on the parametric Riccati equation. The input delay is arbitrarily large and bounded. The asymmetric input saturated system is converted to a switched system with symm...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2019-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8726342/ |