Optimization and control of cyber-physical vehicle systems

JM Bradley, EM Atkins - Sensors, 2015 - mdpi.com
A cyber-physical system (CPS) is composed of tightly-integrated computation,
communication and physical elements. Medical devices, buildings, mobile devices, robots …

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 …

Finite-time attitude tracking control of spacecraft with application to attitude synchronization

H Du, S Li, C Qian - IEEE Transactions on Automatic Control, 2011 - ieeexplore.ieee.org
This note investigates the finite-time attitude control problems for a single spacecraft and
multiple spacecraft. First of all, a finite-time controller is designed to solve finite-time attitude …

[BOEK][B] Analytical mechanics of space systems

H Schaub, JL Junkins - 2003 - books.google.com
Analytical Mechanics of Space Systems by Hanspeter Schaub and John Junkins is a
comprehensive treatment of a stimulating and challenging subject that is both old and new …

Fixed-time attitude tracking control for rigid spacecraft

AM Zou, KD Kumar, AHJ de Ruiter - Automatica, 2020 - Elsevier
The problem of fixed-time attitude tracking control for rigid spacecraft is addressed in this
paper. Based on the backstep** technique and the idea of “adding a power integrator”, a …

Leader–follower cooperative attitude control of multiple rigid bodies

DV Dimarogonas, P Tsiotras, KJ Kyriakopoulos - Systems & Control Letters, 2009 - Elsevier
In this paper we extend our previous results on coordinated control of rotating rigid bodies to
the case of teams with heterogeneous agents. We assume that only a certain subgroup of …

Inverse optimal stabilization of a rigid spacecraft

M Krstic, P Tsiotras - IEEE Transactions on Automatic Control, 1999 - ieeexplore.ieee.org
The authors present an approach for constructing optimal feedback control laws for
regulation of a rotating rigid spacecraft. They employ the inverse optimal control approach …

Fixed-time attitude tracking control for spacecraft with input quantization

H Sun, L Hou, G Zong, X Yu - IEEE Transactions on Aerospace …, 2018 - ieeexplore.ieee.org
This paper investigates the fixed-time attitude tracking control problem for rigid spacecraft
with input quantization and external disturbances. A novel fixed-time disturbance observer is …

Further passivity results for the attitude control problem

P Tsiotras - IEEE Transactions on Automatic Control, 1998 - ieeexplore.ieee.org
In this paper we establish passivity for the system which describes the attitude motion of a
rigid body in terms of minimal three-dimensional kinematic parameters. In particular, we …

Finite-time attitude stabilization for a spacecraft using homogeneous method

H Du, S Li - Journal of Guidance, Control, and Dynamics, 2012 - arc.aiaa.org
The global finite-time attitude stabilization problem for a rigid spacecraft system is
investigated. The actuator saturation is explicitly taken into account in the proposed finite …