Robust fault-tolerant tracking control for spacecraft proximity operations using time-varying sliding mode

Q Hu, X Shao, WH Chen - IEEE Transactions on Aerospace …, 2017 - ieeexplore.ieee.org
The capture of a free-floating tumbling object using an autonomous vehicle is a key
technology for many future orbital missions. Spacecraft proximity operations will play an …

Model predictive control for autonomous rendezvous and docking with a tumbling target

Q Li, J Yuan, B Zhang, C Gao - Aerospace Science and Technology, 2017 - Elsevier
In this paper, we investigate the application of model predictive control (MPC) strategy for
controlling a chaser spacecraft to dock with a tumbling target in space. The CW-based …

Coupled Dynamics and Integrated Control for position and attitude motions of spacecraft: a survey

F Zhang, G Duan - IEEE/CAA journal of Automatica sinica, 2023 - ieeexplore.ieee.org
Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

Receding horizon guidance and control using sequential convex programming for spacecraft 6-DOF close proximity

D Zhou, Y Zhang, S Li - Aerospace Science and Technology, 2019 - Elsevier
This paper presents a receding horizon implementation of sequential convex programming
for the spacecraft six-degree-of-freedom close proximity to a non-cooperative target satellite …

[PDF][PDF] Nonlinear model predictive control for spacecraft rendezvous and docking with a rotating target

H Park, R Zappulla, C Zagaris… - 27th AAS/AIAA …, 2017 - researchgate.net
In this paper, we develop a nonlinear model predictive control (NMPC) approach for
spacecraft rendezvous and docking (RVD) with a rotating target platform. A strategy to …

Minimum-time reconfiguration maneuvers of satellite formations using perturbation forces

D Spiller, F Curti, C Circi - Journal of Guidance, Control, and Dynamics, 2017 - arc.aiaa.org
A novel approach for minimum-time reconfiguration of satellite formations is proposed
considering the perturbation forces as control variables. Planning appropriate attitude …

Autonomous relative navigation using stereo-vision in a dual-agent system for proximity operations in a lunar orbit

E Shepherdson, A de Ruiter, G Liu - Advances in Space Research, 2024 - Elsevier
This paper presents a novel autonomous relative navigation architecture for inspector
spacecraft in proximity operations to a known structure in a lunar orbit. Autonomous on-orbit …

Concurrent proximity control of servicing spacecraft with an uncontrolled target

Q Hu, W Chen, Y Zhang - IEEE/ASME Transactions on …, 2019 - ieeexplore.ieee.org
This paper investigates the six-degrees-of-freedom (6-DOF) rendezvous and docking issue
with an uncontrolled target for a servicing spacecraft under thruster misalignment and …

Cutting-edge trajectory optimization through quantum annealing

A Carbone, F De Grossi, D Spiller - Applied Sciences, 2023 - mdpi.com
This paper introduces an innovative approach to explore the capabilities of Quantum
Annealing (QA) for trajectory optimization in dynamic systems. The proposed method …

Artificial potential function safety and obstacle avoidance guidance for autonomous rendezvous and docking with noncooperative target

J Liu, H Li - Mathematical Problems in Engineering, 2019 - Wiley Online Library
The problem of artificial potential function (APF) safety and obstacle avoidance guidance for
autonomous rendezvous and docking of chaser spacecraft with noncooperative spacecraft …