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 …
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 …
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 …
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 …
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 …
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 …
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 …
A finite-time attitude tracking control scheme is proposed for spacecraft using terminal sliding mode and Chebyshev neural network (NN)(CNN). The four-parameter …
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 …