Aerospace (Jan 2024)

Asynchronously <i>H</i><sub>∞</sub> Tracking Control and Optimization for Switched Flight Vehicles with Time-Varying Delay

  • Xing Yang,
  • Bin Fu,
  • Xiaochuan Ma,
  • Yu Liu,
  • Dongyu Yuan,
  • Xintong Wu

DOI
https://doi.org/10.3390/aerospace11020107
Journal volume & issue
Vol. 11, no. 2
p. 107

Abstract

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The current paper verifies the asynchronous H∞ control and optimization problem for flight vehicles with a time-varying delay. The nonlinear dynamic model and Jacobian linearization establish the flight vehicle’s switched model. An asynchronous H∞ tracking controller is designed, considering the existing asynchronous switching between the controllers and corresponding subsystems. In order to promote transient efficiency, the tracking controller comprises the model-based part and the learning-based part. The model-based part guarantees stability and prescribed efficiency, and the learning-based part compensates for undesirable uncertainties. The multiple Lyapunov function (MLF) and mode-dependent average dwell time (MDADT) methods are utilized to guarantee stability and the specified attenuation efficiency. The existing conditions and the solutions of model-based sub-controllers are represented by linear matrix inequalities (LMIs). The deep Q learning (DQL) algorithm provides the learning-based part. Different from the conventional method, the controller parameters are scheduled online. Therefore, robustness, stability, and dynamic efficiency can be met simultaneously. A numerical example illustrates the efficiency and advantage of the presented approach.

Keywords