DocumentCode
2199141
Title
Analysis of formation flying control of a pair of nano-satellites
Author
Veres, S.M. ; Gabriel, S.B. ; Rogers, E. ; Mayne, D.Q.
Author_Institution
Sch. Eng. Sci., Univ. of Southampton, Highfield, UK
Volume
2
fYear
2001
fDate
2001
Firstpage
1095
Abstract
Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair
Keywords
controllability; linear systems; matrix algebra; nonlinear control systems; position control; set theory; space vehicles; state feedback; constrained control problems; differential drag; disturbances; formation flying control; magnitude constraints; maneuver control; measurement errors; nano-satellites; propulsion; stabilization; Computer science; Educational institutions; Extraterrestrial measurements; Master-slave; Motion control; Position measurement; Propulsion; Satellites; Space stations; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location
Orlando, FL
Print_ISBN
0-7803-7061-9
Type
conf
DOI
10.1109/.2001.981031
Filename
981031
Link To Document