The reducibility of linear second-order time-varying systems with control and observation

被引:10
作者
Kalenova, V. I.
Morozov, V. M.
机构
来源
PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS | 2012年 / 76卷 / 04期
基金
俄罗斯基础研究基金会;
关键词
ORBITS;
D O I
10.1016/j.jappmathmech.2012.09.008
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
The possibility of reducing a linear non-autonomous system, containing a control and measurements, to a time-independent form using time-dependent linear transformations of the state, control and observation spaces is investigated. Second-order systems, that is, systems with a second derivative with respect to time, explicitly present in the equations of motion, are examined. The motion of a spacecraft in the neighbourhood of a libration point under the action of a controlling light pressure force is considered as an application, as well as the problem of determining the orientation of an artificial Earth satellite using solar sensing element measurements. In the first problem, controllability and, in the second case, observability is established by reducing the equations to a time-independent form. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:413 / 422
页数:10
相关论文
共 23 条
[1]  
[Anonymous], 1969, Topics in Mathematical System Theory
[2]  
[Anonymous], 1959, The Theory of Matrices
[3]   Light-Levitated Geostationary Cylindrical Orbits Are Feasible [J].
Baig, Shahid ;
McInnes, Colin R. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (03) :782-793
[4]  
Beletskii, 1965, MOTION SATELLITE ITS
[5]  
Bellman T, 1960, INTRO MATRIX ANAL
[6]   Control of Lagrange point orbits using solar sail propulsion [J].
Bookless, John ;
McInnes, Colin .
ACTA ASTRONAUTICA, 2008, 62 (2-3) :159-176
[7]   AN ALGEBRAIC CHARACTERIZATION OF CONTROLLABILITY [J].
CHANG, A .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1965, AC10 (01) :112-&
[8]  
CHEN CT, 1968, IEEE T AUTOMAT CONTR, VAC13, P195
[9]  
Duboshin G. N., 1968, Celestial Mechanics. Fundamental Problems and Methods
[10]  
Kalenova VI, 2010, LINEAR TIME VARYING