| Citation: | GONG Zheng, LI Peijin, WANG Zian, et al. Design of short landing control strategy for thrust-vectored V/STOL aircraft[J]. Journal of Aerospace Power, 2023, 38（8）：1875-1888 doi: 10.13224/j.cnki.jasp.20210718
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A method to design the landing strategy for vertical/short takeoff and landing vehicles (V/STOL) was established for the shipborne rolling vertical landing (SRVL) process. A longitudinal dynamic model of the protype V/STOL aircraft was established, and then the boundaries of the strategy parameters were determined using attainable balance set methods, on the basis of the deceleration performance, trajectory stability and airspeed stability. The criterion of the strategy parameters specification was also given. Then the control scheme of the strategy was piecewise constructed, where the dynamic inverse methods were applied to the inner loop. A frequency-domain-based control allocation criterion was introduced into this architecture to design the control allocator. Finally, this strategy was verified by Monte Carlo simulations for its robustness performance. The results showed that: the formulation method for strategy parameter boundaries of each landing stages satisfied their requirements respectively, and these parameter boundaries had explicit reference significance to the landing strategy formulation. The landing strategy using L1 adaptive theory for inner loop stability augmentation enables the aircrafts to have excellent trajectory robustness performance.
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