TY - GEN
T1 - Hierarchical Distributed Fixed-Wing Close Formation Management and Control with Erratic UAV Failure
AU - Wei, Qi
AU - Yang, Dongxiao
AU - Zhang, Sheng
AU - Li, Juan
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - Close formation flight of UAVs under erratic conditions enhances collaborative defense and concentrated attacks, yielding air superiority and offensive advantages that present significant threats to adversarial air defense systems. This paper investigates a close formation management and control resolution for fixed-wing UAVs with erratic UAV failure, which has three contributions: Initially, a hierarchical distributed close formation control framework is designed, markedly improving robustness and adaptability compared to conventional centralized leader-follower paradims. Then, a formation management strategy based on Dynamic Spanning Tree (DST) is proposed, to maintain formation density without considering formation shape. Finally, an Adaptive Velocity Tracking (AVT) controller with a roll maneuver adjuster is developed, allowing the close formation to flexibly respond to maneuvering tasks. Validated by UAV swarm simulation with unpredictable node failure, the proposed method meets basic requirements for fixed-wing close formation flight, confirming its feasibility and practicality.
AB - Close formation flight of UAVs under erratic conditions enhances collaborative defense and concentrated attacks, yielding air superiority and offensive advantages that present significant threats to adversarial air defense systems. This paper investigates a close formation management and control resolution for fixed-wing UAVs with erratic UAV failure, which has three contributions: Initially, a hierarchical distributed close formation control framework is designed, markedly improving robustness and adaptability compared to conventional centralized leader-follower paradims. Then, a formation management strategy based on Dynamic Spanning Tree (DST) is proposed, to maintain formation density without considering formation shape. Finally, an Adaptive Velocity Tracking (AVT) controller with a roll maneuver adjuster is developed, allowing the close formation to flexibly respond to maneuvering tasks. Validated by UAV swarm simulation with unpredictable node failure, the proposed method meets basic requirements for fixed-wing close formation flight, confirming its feasibility and practicality.
KW - Fixed-wing UAVs
KW - close formation control
KW - graph theory
KW - hierarchical distributed system
UR - https://www.scopus.com/pages/publications/105031100369
U2 - 10.1109/ISAES66870.2025.11274348
DO - 10.1109/ISAES66870.2025.11274348
M3 - Conference contribution
AN - SCOPUS:105031100369
T3 - 2025 4th International Symposium on Aerospace Engineering and Systems, ISAES 2025
SP - 180
EP - 188
BT - 2025 4th International Symposium on Aerospace Engineering and Systems, ISAES 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 4th International Symposium on Aerospace Engineering and Systems, ISAES 2025
Y2 - 25 July 2025 through 27 July 2025
ER -