Controllability Analysis of Linear Time-Varying T-H Equation with Matrix Sequence Method

Author:

Liu Sihui1ORCID,Huang Qingdao1ORCID

Affiliation:

1. School of Mathematics, Jilin University, Changchun 130000, China

Abstract

A satellite is considered to be moving relative to a nominal elliptical orbit, whose dynamics are usually described by the Tschaunner-Hempel equation (T-H equation). In this paper, we propose to transform the second-order time-varying system represented by the linear T-H equation with a second-order matrix form into a first-order time-varying system. Then, the controllability of the first-order time-varying system is investigated with the matrix sequence method including e = 0 . Meanwhile, we study the observability of the first-order time-varying system with a specific form of measurement. The advantages of the matrix sequence method for controllability and observability analysis are tested by numerical examples, respectively. Dual theory is used to investigate the controllability and observability of the corresponding dual system of the T-H equation. The corresponding conclusions are obtained.

Funder

National Natural Science Foundation of China

Publisher

Hindawi Limited

Subject

Aerospace Engineering

Reference22 articles.

1. Satellite trajectory model reference output tracking control based on TH equation;Y. M. Fu;Journal of Astronautics,2013

2. Terminal Guidance System for Satellite Rendezvous

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4. Nonlinear Dynamic Equations of Satellite Relative Motion Around an Oblate Earth

5. Optimale Beschleunigeungs programme fur das Rendezvous-Manover;J. Tschauner;Astronautica Acta,1964

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