Dynamic Soaring Trajectory Optimization Considering the Path Following Performance

Dynamic soaring is a technique employed by some kinds of birds to extract energy by intelligently flying in shear wind. The combination of trajectory optimization and path following is currently the most used duo in real-world application of dynamic soaring. However, the separate design of the trajectory and the controller inherently introduces a fair degree of conservativeness, compromising optimality. In this study, we propose a dynamic soaring trajectory optimization algorithm, which additionally considers the closed-loop stabilization of the path following error dynamics through gain scheduling. In other words, the stability of the path-deviation error controller is taken into account through the Routh criterion already in the form of constraints when designing the trajectory in the optimization problem. Consequently, the optimized dynamic soaring trajectory as well as the feedback gains are obtained simultaneously by solving the trajectory optimization problem. The proposed algorithm balances optimality and stability and thereby reduces conservativeness. Eventually, simulations demonstrate the effectiveness of the algorithm.

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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2025-02-21
DOI
https://doi.org/10.1109/taes.2025.3544581
Citations
1
Primary Topic
Vehicle Dynamics and Control Systems
Type
article
Field-Weighted Citation Impact
0.68

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Dynamic Soaring Trajectory Optimization Considering the Path Following Performance

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article

Dynamic Soaring Trajectory Optimization Considering the Path Following Performance

Alexander Zwenig, Patrick Piprek, Haichao Hong, Florian Holzapfel, Xueqing Nie
article en
1 citations

Abstract

Dynamic soaring is a technique employed by some kinds of birds to extract energy by intelligently flying in shear wind. The combination of trajectory optimization and path following is currently the most used duo in real-world application of dynamic soaring. However, the separate design of the trajectory and the controller inherently introduces a fair degree of conservativeness, compromising optimality. In this study, we propose a dynamic soaring trajectory optimization algorithm, which additionally considers the closed-loop stabilization of the path following error dynamics through gain scheduling. In other words, the stability of the path-deviation error controller is taken into account through the Routh criterion already in the form of constraints when designing the trajectory in the optimization problem. Consequently, the optimized dynamic soaring trajectory as well as the feedback gains are obtained simultaneously by solving the trajectory optimization problem. The proposed algorithm balances optimality and stability and thereby reduces conservativeness. Eventually, simulations demonstrate the effectiveness of the algorithm.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(4)
Shanghai Jiao Tong University (CN), Technical University of Munich (DE)
National Natural Science Foundation of China, Natural Science Foundation of Sichuan Province
Climate action
Openalex Percentile: Top 34%
Vehicle Dynamics and Control Systems
0.68
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