Volume 39 Issue 4
Apr.  2024
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DAN Zhihong, ZHANG Song, ZHANG Hehong, et al. Robust cascade LADRC technology for flight altitude simulation of high altitude cell[J]. Journal of Aerospace Power, 2024, 39(4):20220343 doi: 10.13224/j.cnki.jasp.20220343
Citation: DAN Zhihong, ZHANG Song, ZHANG Hehong, et al. Robust cascade LADRC technology for flight altitude simulation of high altitude cell[J]. Journal of Aerospace Power, 2024, 39(4):20220343 doi: 10.13224/j.cnki.jasp.20220343

Robust cascade LADRC technology for flight altitude simulation of high altitude cell

doi: 10.13224/j.cnki.jasp.20220343
  • Received Date: 2022-05-16
    Available Online: 2023-09-12
  • With strong nonlinearity, high uncertainty and strong external disturbance for flight altitude simulation of altitude test facility, a robust cascade linear active disturbance rejection control (LADRC) algorithm via the reduced order linear extended state observer (RLESO) was proposed. In particular, the main characteristics and control issues of the controlled plant were analyzed, and the generalized controlled plant can be included by the butterfly valve position loop and flight altitude loop. The RLESO and corresponding controller were designed for the two loops respectively, meanwhile the cascade control system was constructed. The robust cascade LADRC was realized in the simulation environment and compared with the classical PID control scheme. When the engine was subject to the thrust transient test, the maximum fluctuation value of the controlled pressure was reduced from 3.5 kPa to 0.8 kPa. This indicated that the robust cascade LADRC technology via RLESO can significantly improve the dynamic control quality. The ideal robust control performance and anti-disturbance ability for flight altitude simulation were obtained.


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