TY - JOUR
T1 - An Adaptive Re-Entry Spatial–Temporal Cooperative Guidance Method Under Optimal Topology
AU - Zhu, Jianwen
AU - Wang, Xiafu
AU - Yu, Jianglong
AU - Feng, Zhi
AU - Dong, Xiwang
N1 - Publisher Copyright:
Copyright © 2026 Jianwen Zhu et al. International Journal of Aerospace Engineering published by John Wiley & Sons Ltd.
PY - 2026
Y1 - 2026
N2 - This paper addresses the adaptive spatiotemporal cooperative guidance problem for high-velocity vehicles independent of standard trajectories by proposing a strategy that combines the gliding and diving-down phases under an optimal topology. For the impact time and angle control guidance (ITACG) of individual vehicles, lateral maneuvering is introduced to control the arrival time, complementing an optimal guidance law that enforces terminal position and angle constraints. The maneuvering amplitude in the gliding phase and the maneuvering duration in the diving-down phase are determined online via a prediction–correction approach. Regarding cooperative guidance, a two-layer structure is constructed, consisting of individual guidance at the bottom layer and cooperative guidance at the upper layer. In the upper layer, the coordinated variable is calculated using a consensus method, and the network topology is optimized to minimize communication cost. At the methodological level, the simulation results show that the proposed guidance achieves a terminal position error of less than 1 m, an angle error of less than 0.01°, and a time error of less than 1 s.
AB - This paper addresses the adaptive spatiotemporal cooperative guidance problem for high-velocity vehicles independent of standard trajectories by proposing a strategy that combines the gliding and diving-down phases under an optimal topology. For the impact time and angle control guidance (ITACG) of individual vehicles, lateral maneuvering is introduced to control the arrival time, complementing an optimal guidance law that enforces terminal position and angle constraints. The maneuvering amplitude in the gliding phase and the maneuvering duration in the diving-down phase are determined online via a prediction–correction approach. Regarding cooperative guidance, a two-layer structure is constructed, consisting of individual guidance at the bottom layer and cooperative guidance at the upper layer. In the upper layer, the coordinated variable is calculated using a consensus method, and the network topology is optimized to minimize communication cost. At the methodological level, the simulation results show that the proposed guidance achieves a terminal position error of less than 1 m, an angle error of less than 0.01°, and a time error of less than 1 s.
KW - ITACG
KW - cooperative guidance
KW - high-velocity vehicle
KW - optimal topology
KW - spatiotemporal consistency
UR - https://www.scopus.com/pages/publications/105033854400
U2 - 10.1155/ijae/2636385
DO - 10.1155/ijae/2636385
M3 - 文章
AN - SCOPUS:105033854400
SN - 1687-5966
VL - 2026
JO - International Journal of Aerospace Engineering
JF - International Journal of Aerospace Engineering
IS - 1
M1 - 2636385
ER -