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Open Access

Optimal trajectory design accounting for the stabilization of linear time-varying error dynamics

Patrick PIPREKaHaichao HONGa( )Florian HOLZAPFELa
Institute of Flight System Dynamics, Technical University of Munich, Garching D-85748, Germany
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Abstract

This study is dedicated to the development of a direct optimal control-based algorithm for trajectory optimization problems that accounts for the closed-loop stability of the trajectory tracking error dynamics already during the optimization. Consequently, the trajectory is designed such that the Linear Time-Varying (LTV) dynamic system, describing the controller’s error dynamics, is stable, while additionally the desired optimality criterion is optimized and all enforced constraints on the trajectory are fulfilled. This is achieved by means of a Lyapunov stability analysis of the LTV dynamics within the optimization problem using a time-dependent, quadratic Lyapunov function candidate. Special care is taken with regard to ensuring the correct definiteness of the ensuing matrices within the Lyapunov stability analysis, specifically considering a numerically stable formulation of these in the numerical optimization. The developed algorithm is applied to a trajectory design problem for which the LTV system is part of the path-following error dynamics, which is required to be stable. The main benefit of the proposed scheme in this context is that the designed trajectory trades-off the required stability and robustness properties of the LTV dynamics with the optimality of the trajectory already at the design phase and thus, does not produce unstable optimal trajectories the system must follow in the real application.

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Chinese Journal of Aeronautics
Pages 55-66

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Cite this article:
PIPREK P, HONG H, HOLZAPFEL F. Optimal trajectory design accounting for the stabilization of linear time-varying error dynamics. Chinese Journal of Aeronautics, 2022, 35(7): 55-66. https://doi.org/10.1016/j.cja.2021.10.031

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Received: 28 April 2021
Revised: 06 June 2021
Accepted: 29 June 2021
Published: 23 November 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).