Spacecraft Attitude and Orbit Coupled Nonlinear Adaptive Synchronization Control

Yu Jia Tie; Wei Yang; Hao Yu Tan

doi:10.4028/www.scientific.net/AMR.327.6

Paper Titles

Preface and Corganizing Committee

Stability Study of the Geogrids Reinforced Tailings
p.1

Spacecraft Attitude and Orbit Coupled Nonlinear Adaptive Synchronization Control
p.6

A New Adaptive Fuzzy Sliding Mode Control for Uncertain Nonlinear Systems
p.12

The Application of ADRC in the Ship Main Engine Speed Controller Based on Genetic Algorithm
p.17

Synthesis and Properties of a New Diarylethene with Two Different Substituents for Optical Recording
p.23

Synthesis and Fluorescence Switching of a Photochromic Diarylethene Bearing Chlorine Atoms
p.27

Application of Skin Detection Based on Irregular Polygon Area Boundary Constraint on YCbCr and Reverse Gamma Correction
p.31

A Photochromic Diarylethene with Five and Six-Membered Aryl Units
p.37

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 327Spacecraft Attitude and Orbit Coupled Nonlinear...

Spacecraft Attitude and Orbit Coupled Nonlinear Adaptive Synchronization Control

Abstract:

Precise dynamic model of spacecraft is essential for the space missions, to be completed successfully. Nevertheless, the independent orbit or attitude dynamic models can not meet high precision tasks. This paper developed a 6-DOF relative coupling dynamic model based upon the nonlinear relative motion dynamics equations and attitude kinematics equations described by MRP. Nonlinear synchronization control law was designed for the coupled nonlinear dynamic model, whose close-loop system was proved to be global asymptotic stable by Lyapunov direct method. Finallly, the simulation results illustrate that the nonlinear adaptive synchronization control algorithm can robustly drive the orbit and attitude errors to converge to zero.

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Periodical:

Advanced Materials Research (Volume 327)

Pages:

6-11

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.327.6

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Online since:

September 2011

Authors:

Yu Jia Tie, Wei Yang, Hao Yu Tan

Keywords:

Adaptive Control, Attitude Coupling Model, Modified Rodrigues Parameters, Nonlinear Control, Orbital Coupling Model, Quasi-Lagrange Equation, Synchronization Control

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