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Volume 50 Issue 5
May  2024
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Journal of Beijing University of Aeronautics and Astronautics  > 2024  >  50(5): 1576-1585.
ZHEN X D，WANG Z A，HU R C，et al. Aircraft flight qualities of short take-off and vertical landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1576-1585 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0413
Citation: ZHEN X D，WANG Z A，HU R C，et al. Aircraft flight qualities of short take-off and vertical landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1576-1585 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0413
shu

Aircraft flight qualities of short take-off and vertical landing

doi: 10.13700/j.bh.1001-5965.2022.0413
  • 1.

    College of Aerospace Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 210000，China

  • 2.

    China Academy of Launch Vehicle Technology，Beijing 100076，China

Funds:  National Natural Science Foundation of China (11402115)
More Information
  • Corresponding author: E-mail：chenyl79@nuaa.edu.cn
  • Received Date: 26 May 2022
  • Accepted Date: 25 Jun 2022
    • Available Online: 16 Sep 2022
  • Publish Date: 14 Sep 2022
    Abstract

  • Based on the characteristics of short take-off and vertical landing (STOVL) aircraft, the flight quality requirements of STOVL aircraft are proposed in light of control efficiency and modal characteristics, combined with the AGARD 577 flight quality specification. The control efficiency of the vehicle in the transition state of STOVL is evaluated based on the STOVL 6-DOF model simulation. Drawing on the concept of equivalent system matching, the hybrid algorithm of the genetic algorithm and least square method is used to carry out low order equivalent matching of high order aircraft model with L1 adaptive controller. Using this low order model, the modal characteristics of the vehicle in longitudinal and lateral directions are evaluated. The evaluation demonstrates the first-class flight quality of the aircraft in STOVL .

     

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