Comprehensive survey and assessment of spacecraft relative motion dynamics models

J Sullivan, S Grimberg, S D'Amico - Journal of Guidance, Control, and …, 2017 - arc.aiaa.org
IN THE framework of spacecraft relative motion, current dynamics models are diverse and
often subject to a multitude of constraints and limitations on the intersatellite range of …

Spacecraft formation flying: a review and new results on state feedback control

R Kristiansen, PJ Nicklasson - Acta Astronautica, 2009 - Elsevier
This paper presents a review of previous work within the field of spacecraft formation flying,
including modeling approaches and controller design. In addition, five new approaches for …

Deep reinforcement learning for six degree-of-freedom planetary landing

B Gaudet, R Linares, R Furfaro - Advances in Space Research, 2020 - Elsevier
This work develops a deep reinforcement learning based approach for Six Degree-of-
Freedom (DOF) planetary powered descent and landing. Future Mars missions will require …

Distributed finite-time attitude containment control for multiple rigid bodies

Z Meng, W Ren, Z You - Automatica, 2010 - Elsevier
Distributed finite-time attitude containment control for multiple rigid bodies is addressed in
this paper. When there exist multiple stationary leaders, we propose a model-independent …

[图书][B] Optimal estimation of dynamic systems

JL Crassidis, JL Junkins - 2004 - taylorfrancis.com
Most newcomers to the field of linear stochastic estimation go through a difficult process in
understanding and applying the theory. This book minimizes the process while introducing …

[图书][B] Spacecraft formation flying: Dynamics, control and navigation

K Alfriend, SR Vadali, P Gurfil, J How, L Breger - 2009 - books.google.com
Space agencies are now realizing that much of what has previously been achieved using
hugely complex and costly single platform projects—large unmanned and manned satellites …

[图书][B] Statistical orbit determination

B Schutz, B Tapley, GH Born - 2004 - books.google.com
Statistical Orbit Determination presents fundmentals of orbit determination--from weighted
least squares approaches (Gauss) to today's high-speed computer algorithms that provide …

Survey of nonlinear attitude estimation methods

JL Crassidis, FL Markley, Y Cheng - Journal of guidance, control, and …, 2007 - arc.aiaa.org
ATTITUDE estimation involves a two-part process: 1) estimation of a vehicle's orientation
from body measurements and known reference observations, such as line-of-sight …

Finite-time attitude tracking control for spacecraft using terminal sliding mode and Chebyshev neural network

AM Zou, KD Kumar, ZG Hou… - IEEE Transactions on …, 2011 - ieeexplore.ieee.org
A finite-time attitude tracking control scheme is proposed for spacecraft using terminal
sliding mode and Chebyshev neural network (NN)(CNN). The four-parameter …

Generic smoothing for optimal bang-off-bang spacecraft maneuvers

E Taheri, JL Junkins - Journal of Guidance, Control, and Dynamics, 2018 - arc.aiaa.org
THE field of trajectory optimization has a rich history dating back to 1950s. Traditionally,
these problems are solved by direct and indirect methods with their advantages and …