TY - GEN
T1 - Trajectory planning and control for a multilift system based on load distribution
AU - Geng, Junyi
AU - Singla, Puneet
AU - Langelaan, Jack W.
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - This paper studies a load distribution based trajectory planning and control strategy for a hierarchically-controlled multilift system. It proposes a method that simultaneously plans payload trajectory and cable forces while satisfying path and force constraints and minimizing the difference in cable forces. A direct collocation method is used to solve the formulated planning problem. Then, a neighboring feedback law is designed to equalize the cable tension load distribution during flight. Here, small perturbation is performed to linearize the system with respect to the nominal path. An LQR controller is then designed for the system to track the planned trajectory. Simulation results showed the system has a good performance even under wind gust environment. The system ended with more evenly distributed cable tension load comparing with the case without planning based on the load distribution.
AB - This paper studies a load distribution based trajectory planning and control strategy for a hierarchically-controlled multilift system. It proposes a method that simultaneously plans payload trajectory and cable forces while satisfying path and force constraints and minimizing the difference in cable forces. A direct collocation method is used to solve the formulated planning problem. Then, a neighboring feedback law is designed to equalize the cable tension load distribution during flight. Here, small perturbation is performed to linearize the system with respect to the nominal path. An LQR controller is then designed for the system to track the planned trajectory. Simulation results showed the system has a good performance even under wind gust environment. The system ended with more evenly distributed cable tension load comparing with the case without planning based on the load distribution.
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M3 - Conference contribution
AN - SCOPUS:85100298659
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 15
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -