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 …

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 …

Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers

J Virgili-Llop, C Zagaris, H Park, R Zappulla… - CEAS Space …, 2018 - Springer
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 …

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.” …

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 …

A near-optimal guidance for cooperative docking maneuvers

M Ciarcia, A Grompone, M Romano - Acta Astronautica, 2014 - Elsevier
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 …

Performance evaluation of the inverse dynamics method for optimal spacecraft reorientation

J Ventura, M Romano, U Walter - Acta Astronautica, 2015 - Elsevier
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 …

A direct method-based suboptimal attitude guidance for accurate ground-target tracking maneuvers

G Lavezzi, M Ciarcià - Advances in Space Research, 2022 - Elsevier
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 …

Attitude control strategies for an imaging cubesat

G Lavezzi, ME Grøttey, M Ciarcià - 2019 IEEE International …, 2019 - ieeexplore.ieee.org
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 …

[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 …