Study on Gain-Scheduled Control of a High-Speed Variable-Sweep Vehicle

Variations in flight conditions and wing configuration alter the aerodynamic characteristics and inertial properties of high-speed variable-sweep vehicles. A longitudinal gain-scheduled controller combining common Lyapunov vertex synthesis and inverse-distance weighting (IDW) is investigated. A normalized effective interpolation distance bounds the deviation from the nearest vertex gain and yields a sufficient stability condition for an ideal scheduled short-period model under regularity and covering-radius assumptions. Numerical simulations show that IDW is defined at all 2000 sampled operating points, with Hurwitz-stable frozen models, whereas barycentric interpolation covers 33.9%. Compared with the parameter-dependent Lyapunov function (PDLF)-based barycentric baseline, the weighted nominal tracking score differs by 0.56%, and both controllers pass 298 of 300 perturbed simulations. Mean full-simulation elapsed time decreases from 238.3 to 59.4 s, a 75.1% reduction in the tested MATLAB implementation. These results support broader sampled coverage and comparable tracking performance with lower implementation-specific computational cost.

Authors

Publication Details

Journal
Aerospace
Published
2026-11-10
DOI
https://doi.org/10.3390/aerospace13111054
Primary Topic
Aerospace Engineering and Control Systems
Type
article
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article

Study on Gain-Scheduled Control of a High-Speed Variable-Sweep Vehicle

Chunlei Xie, Zhifan Gong, Yufei Han, Jianyu Zan et al.
Aerospace
Aerospace Engineering and Control Systems
article

Study on Gain-Scheduled Control of a High-Speed Variable-Sweep Vehicle

Chunlei Xie, Zhifan Gong, Yufei Han, Jianyu Zan, Xuhui Zhang
article en

Abstract

Variations in flight conditions and wing configuration alter the aerodynamic characteristics and inertial properties of high-speed variable-sweep vehicles. A longitudinal gain-scheduled controller combining common Lyapunov vertex synthesis and inverse-distance weighting (IDW) is investigated. A normalized effective interpolation distance bounds the deviation from the nearest vertex gain and yields a sufficient stability condition for an ideal scheduled short-period model under regularity and covering-radius assumptions. Numerical simulations show that IDW is defined at all 2000 sampled operating points, with Hurwitz-stable frozen models, whereas barycentric interpolation covers 33.9%. Compared with the parameter-dependent Lyapunov function (PDLF)-based barycentric baseline, the weighted nominal tracking score differs by 0.56%, and both controllers pass 298 of 300 perturbed simulations. Mean full-simulation elapsed time decreases from 238.3 to 59.4 s, a 75.1% reduction in the tested MATLAB implementation. These results support broader sampled coverage and comparable tracking performance with lower implementation-specific computational cost.

AerospaceVol. 13(11)
Aerospace Engineering and Control Systems
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