Author(s):
Guerman, Anna 
; Smirnov, Georgi
Date: 2012
Persistent ID: http://hdl.handle.net/1822/21183
Origin: RepositóriUM - Universidade do Minho
Document details
Orbital manoeuvres with single-input control
Description
We study the problem of orbital control under the constraints on the thrust direction for a nonlinear dynamical model. The satellite is equipped with a passive attitude control system providing one-axis stabilization and a propulsion system consisting of one or two thrusters oriented along the stabilized axis. Different applications, such as formation flying and satellite de-orbiting are considered.
We study the problem of orbital control under the constraints on the thrust direction for a nonlinear dynamical model. The satellite is equipped with a passive attitude control system providing one-axis stabilization and a propulsion system consisting of one or two thrusters oriented along the stabilized axis. Different applications, such as formation flying and satellite de-orbiting are considered.
Document Type
Article
Language English
Language English
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