TY - JOUR
T1 - Optimal trajectory design accounting for the stabilization of linear time-varying error dynamics
AU - PIPREK, Patrick
AU - HONG, Haichao
AU - HOLZAPFEL, Florian
N1 - Publisher Copyright:
© 2021 Chinese Society of Aeronautics and Astronautics
PY - 2022/7
Y1 - 2022/7
N2 - 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.
AB - 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.
KW - LTV error dynamics
KW - LTV stability
KW - Optimal control-based LTV stabilization
KW - Path-following error controller
KW - Trajectory generation
KW - Trajectory optimization
UR - http://www.scopus.com/inward/record.url?scp=85126808673&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2021.10.031
DO - 10.1016/j.cja.2021.10.031
M3 - Article
AN - SCOPUS:85126808673
SN - 1000-9361
VL - 35
SP - 55
EP - 66
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 7
ER -