Fixed-time maneuver control of spacecraft autonomous rendezvous with a free-tumbling target
Q Hu, W Chen, L Guo - IEEE Transactions on Aerospace and …, 2018 - ieeexplore.ieee.org
This paper considers the fixed-time translational operation control issue for the spacecraft
rendezvous task with a free-tumbling target. The translation dynamics model of the …
rendezvous task with a free-tumbling target. The translation dynamics model of the …
Guidance and control for multi-stage rendezvous and docking operations in the presence of uncertainty
CM Jewison - 2017 - dspace.mit.edu
Rendezvous and docking missions have been a mainstay of space exploration from the
Apollo program through present day operations with the International Space Station. There …
Apollo program through present day operations with the International Space Station. There …
Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers
An experimental campaign has been conducted to evaluate the performance of two different
guidance and control algorithms on a multi-constrained docking maneuver. The evaluated …
guidance and control algorithms on a multi-constrained docking maneuver. The evaluated …
Experimental characterization of inverse dynamics guidance in docking with a rotating target
M Wilde, M Ciarcià, A Grompone… - Journal of Guidance …, 2016 - arc.aiaa.org
The performance of an inverse dynamics guidance and control strategy is experimentally
evaluated for the planar maneuver of a “chaser” spacecraft docking with a rotating “target.” …
evaluated for the planar maneuver of a “chaser” spacecraft docking with a rotating “target.” …
Optimal guidance and collision avoidance for docking with the rotating target spacecraft
Z Xu, Y Chen, Z Xu - Advances in Space Research, 2019 - Elsevier
The guidance and control strategy for spacecraft rendezvous and docking are of vital
importance, especially for a chaser spacecraft docking with a rotating target spacecraft …
importance, especially for a chaser spacecraft docking with a rotating target spacecraft …
A near-optimal guidance for cooperative docking maneuvers
In this work we study the problem of minimum energy docking maneuvers between two
Floating Spacecraft Simulators. The maneuvers are planar and conducted autonomously in …
Floating Spacecraft Simulators. The maneuvers are planar and conducted autonomously in …
Performance evaluation of the inverse dynamics method for optimal spacecraft reorientation
This paper investigates the application of the inverse dynamics in the virtual domain method
to Euler angles, quaternions, and modified Rodrigues parameters for rapid optimal attitude …
to Euler angles, quaternions, and modified Rodrigues parameters for rapid optimal attitude …
A direct method-based suboptimal attitude guidance for accurate ground-target tracking maneuvers
This work presents an attitude control strategy for Earth-imaging satellites. The proposed
methodology is based on the closed-loop implementation of a direct method and a nonlinear …
methodology is based on the closed-loop implementation of a direct method and a nonlinear …
Attitude control strategies for an imaging cubesat
This paper presents two different attitude control strategies for a fixed target-tracking remote
sensing CubeSat. In particular, the observation mission profile requires the CubeSat to …
sensing CubeSat. In particular, the observation mission profile requires the CubeSat to …
[PDF][PDF] An inverse dynamics approach to the guidance of spacecraft in close proximity of tumbling debris
A Caubet, JD Biggs - detail, 2015 - researchgate.net
This paper proposes a trajectory planning method based on polynomial shaping, applied to
the docking scenario in the framework of an Active Debris Removal mission. A tumbling …
the docking scenario in the framework of an Active Debris Removal mission. A tumbling …