An adaptive surrogate model-based fast planning for swarm safe migration along halo orbit

X Zhou, Y Cheng, D Qiao, Z Huo - Acta Astronautica, 2022 - Elsevier
Taken the optimal assignment, trajectory optimization and collision avoidance into
consideration, this research focuses on the fast-planning method for swarm safe-migration …

Survey on advances in orbital dynamics and control for libration point orbits

M Xu, Y Liang, K Ren - Progress in Aerospace Sciences, 2016 - Elsevier
Libration point orbits (LPOs) have drawn a lot of interest because of their great significance
in deep space exploration. This paper summarizes the past developments and then …

Nonlinear receding horizon guidance for spacecraft formation reconfiguration on libration point orbits using a symplectic numerical method

H Peng, X Jiang - Isa Transactions, 2016 - Elsevier
This paper studies a nonlinear receding horizon control guidance strategy for spacecraft
formation reconfiguration on libration orbits in the Sun–Earth system. For comparison, a …

Formation flying on quasi-halo orbits in restricted Sun–Earth/Moon system

M Xu, Y Liang, X Fu - Aerospace Science and Technology, 2017 - Elsevier
Due to the strong nonlinear perturbations near the libration points, the continuous low-thrust
technique has many potential applications in stationkeeping relative motions. The …

Dynamics of double-pyramid satellite formations interconnected by tethers and coulomb forces

R Qi, AK Misra - Journal of Guidance, Control, and Dynamics, 2016 - arc.aiaa.org
The tethered formation and the coulomb formation are two important concepts in
constructing satellite formation architecture, and they have the advantage that the relative …

Optimal control of loose spacecraft formations near libration points with collision avoidance

M Li, H Peng, W Zhong - Nonlinear Dynamics, 2016 - Springer
This paper investigates the optimal control of loose leader-following spacecraft formations
near libration points. The formation reconfigurations and keepings can be applied at the …

Event-based impulsive control for spacecraft rendezvous hovering phases

JC Sanchez, C Louembet, F Gavilan… - Journal of Guidance …, 2021 - arc.aiaa.org
This work presents an event-triggered controller for spacecraft rendezvous hovering phases.
The goal is to maintain the chaser within a bounded region with respect to the target. The …

Transfer to a multi-revolution elliptic halo orbit in Earth–Moon elliptic restricted three-body problem using stable manifold

H Peng, S Xu - Advances in Space Research, 2015 - Elsevier
Abstract The Multi-revolution Elliptic Halo (ME-Halo) orbit is a special kind of symmetric
periodic orbits generated in the Elliptic Restricted Three-Body Problem (ERTBP). Its special …

Low Frequency Hierarchical Cooperative Impulse Control for Gravitational Wave Detector Formation Keeping

X Xie, F Jiang, J Li - Journal of Guidance, Control, and Dynamics, 2024 - arc.aiaa.org
Configuration stability is crucial for the detection accuracy of space-based gravitational wave
(GW) detectors. This paper proposes a low-frequency hierarchical cooperative impulse …

[PDF][PDF] Impulsive control of formations near invariant tori via local toroidal coordinates

I Elliott, N Bosanac - 32nd AAS/AIAA Astrodynamics Specialist …, 2021 - colorado.edu
Invariant tori relative to periodic orbits have historically been identified as a useful reference
for locating spacecraft formations in multi-body environments. An impulsive control strategy …