Distributed control for satellite cluster flight under different communication topologies

H Zhang, P Gurfil - Journal of Guidance, Control, and Dynamics, 2016 - arc.aiaa.org
Cluster flight algorithms enable the operation of multiple satellites within given distance
bounds for long periods of time. Synchronizing the states of the satellites in the cluster is …

Modeling and co-simulating of a large flexible satellites with three reaction wheels in ADAMS and MATLAB

M Tahmasebi, SM Esmailzadeh - International Journal of Dynamics and …, 2018 - Springer
In this paper, a simple, accurate, and quick approach for modeling and controlling a large
flexible satellite is presented. A satellite including three reaction wheels and two large …

An MPC-based attitude control system for all-electric spacecraft with on/off actuators

M Leomanni, A Garulli, A Giannitrapani… - … IEEE conference on …, 2013 - ieeexplore.ieee.org
Pointing accuracy is a key requirement in communication satellites and Earth observation
missions. Attitude control systems must guarantee tracking of the reference attitude and …

[图书][B] Advanced navigation and guidance for high-precision planetary landing on Mars= Navigation et guidage avancés pour un atterrissage planétaire à haute …

JF Lévesque - 2007 - library-archives.canada.ca
Plusieurs missions internationales prévues pour les années 2011-2013 ont pour objectif le
retour d'échantillons de la planète Mars. Ces missions requièrent un atterrissage précis sur …

Spacecraft attitude dynamics simulator actuated by cold gas propulsion system

M Mirshams, H Taei, M Ghobadi… - Proceedings of the …, 2015 - journals.sagepub.com
This article describes the details of an advanced Spacecraft Attitude Dynamics Simulator
(SADS) at the Space Research Laboratory (SRL) at the KN Toosi University of Technology …

All-electric spacecraft precision pointing using model predictive control

M Leomanni, A Garulli, A Giannitrapani… - Journal of Guidance …, 2015 - arc.aiaa.org
ALL-ELECTRIC spacecraft, using electric propulsion (EP) systems for attitude control, have
been studied since the early 1960s. The potential application of a Teflon pulsed plasma …

[PDF][PDF] From classical absolute stability tests towards a comprehensive robustness analysis

M Fetzer - 2017 - d-nb.info
IN this thesis, we are concerned with the stability and performance anal-ysis of feedback
interconnections comprising a linear (time-invariant) system and an uncertain component …

Effect of seawater exposure on impact damping behavior of viscoelastic material of pounding tuned mass damper (PTMD)

P Zhang, D Patil, SCM Ho - Applied Sciences, 2019 - mdpi.com
The pounding tuned mass damper (PTMD) is a novel vibration control device that can
effectively mitigate the undesired vibration of subsea pipeline structures. Previous studies …

Attitude control schemes for crew module atmospheric re-entry experiment mission

N Soumya, AP Nair, V Brinda, DS Sheela… - IFAC-PapersOnLine, 2018 - Elsevier
Abstract The Crew Module Atmospheric Re-entry Experiment mission is a suborbital mission
of flying Crew Module (CM) as the payload in a parent launch vehicle. After separation from …

Upper-stage launch vehicle servo controller design considering optimal thruster configuration

TW Hwang, CS Park, MJ Tahk, H Bang - AIAA Guidance, Navigation …, 2003 - arc.aiaa.org
An attitude control system using reaction thrusters for the upper stage of a launch vehicle is
considered. The thruster configuration (position and direction) determines control system …