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

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 Li...

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Bibliographic Details
Published inChinese journal of aeronautics Vol. 35; no. 7; pp. 55 - 66
Main Authors PIPREK, Patrick, HONG, Haichao, HOLZAPFEL, Florian
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.07.2022
Institute of Flight System Dynamics,Technical University of Munich,Garching D-85748,Germany
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ISSN1000-9361
2588-9230
DOI10.1016/j.cja.2021.10.031

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Summary: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.
ISSN:1000-9361
2588-9230
DOI:10.1016/j.cja.2021.10.031