Abstract
According to the tracking error of reaction control system (RCS), a new precision control strategy is proposed for the initial reentry phase of reentry vehicle. Firstly, a nonlinear disturbance observer (DOB) is used for observing the model uncertainty and/or external disturbances. Secondly, a sliding mode control system for the fast loop and slow loop is designed by back-stepping style, and obtained the optimal combination of RCS by linear optimization. Besides, a Integral PWPF Modulator (IPWPF) is proposed based on traditional PWPF modulator, and its stability is proved by a describing function. Finally, the simulation indicates a great precision of the method.
Original language | English |
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Pages (from-to) | 511-516 |
Number of pages | 6 |
Journal | Guti Huojian Jishu/Journal of Solid Rocket Technology |
Volume | 40 |
Issue number | 4 |
DOIs | |
State | Published - 1 Aug 2017 |
Keywords
- Disturbance observer
- PWPF modulator
- Reaction control system
- Reentry vehicle
- Sliding mode