TY - GEN
T1 - Consistency Formation Maneuver Control Based on Nonlinear Dynamic Inverse
AU - Wang, Yunhui
AU - Cai, Yunpeng
AU - Han, Yinghua
AU - Shi, Jingping
N1 - Publisher Copyright:
© 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
PY - 2023
Y1 - 2023
N2 - In the process of formation control, the conventional consistent formation control methods often adjust the relative position of each aircraft relative to the formation virtual center node to achieve formation maintenance and control. Its essence is to complete the formation adjustment through the track command. However, it is difficult to achieve effective control for the maneuvering formation control, such as rapid dive, jump and turn, which often appear in the formation performance, and it is easy to show the shortcomings of poor synchronization and poor consistency. Aiming at the problem of maneuvering formation, a consistent formation maneuver control method based on nonlinear dynamic inversion is proposed. Based on the establishment of a basic maneuver action database, the method uses velocity, track angle, and track azimuth as the consistency variables of formation control to realize the control of maneuvering formation. Therefore, it can effectively control the rapid maneuver on the premise of ensuring the formation stability control.
AB - In the process of formation control, the conventional consistent formation control methods often adjust the relative position of each aircraft relative to the formation virtual center node to achieve formation maintenance and control. Its essence is to complete the formation adjustment through the track command. However, it is difficult to achieve effective control for the maneuvering formation control, such as rapid dive, jump and turn, which often appear in the formation performance, and it is easy to show the shortcomings of poor synchronization and poor consistency. Aiming at the problem of maneuvering formation, a consistent formation maneuver control method based on nonlinear dynamic inversion is proposed. Based on the establishment of a basic maneuver action database, the method uses velocity, track angle, and track azimuth as the consistency variables of formation control to realize the control of maneuvering formation. Therefore, it can effectively control the rapid maneuver on the premise of ensuring the formation stability control.
KW - Consistency theory
KW - Maneuver library
KW - Nonlinear dynamic inversion
KW - UAVs formation
UR - https://www.scopus.com/pages/publications/85151117157
U2 - 10.1007/978-981-19-6613-2_126
DO - 10.1007/978-981-19-6613-2_126
M3 - 会议稿件
AN - SCOPUS:85151117157
SN - 9789811966125
T3 - Lecture Notes in Electrical Engineering
SP - 1270
EP - 1281
BT - Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Deng, Yimin
A2 - Yan, Liang
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2022
Y2 - 5 August 2022 through 7 August 2022
ER -