TY - JOUR
T1 - Dynamic Soaring Trajectory Optimization Considering the Path Following Performance
AU - Nie, Xueqing
AU - Zwenig, Alexander
AU - Piprek, Patrick
AU - Holzapfel, Fl ORIAN
AU - Hong, Haichao
N1 - Publisher Copyright:
© 1965-2011 IEEE ALL RIGHT RESERVED.
PY - 2025
Y1 - 2025
N2 - 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 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.
AB - 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 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.
KW - dynamic soaring
KW - stability of path-following error dynamics
KW - trajectory optimization
UR - http://www.scopus.com/inward/record.url?scp=85218729751&partnerID=8YFLogxK
U2 - 10.1109/TAES.2025.3544581
DO - 10.1109/TAES.2025.3544581
M3 - Article
AN - SCOPUS:85218729751
SN - 0018-9251
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
ER -