Station-keeping and formation flying based on nonlinear output regulation theory-Reference-Cited by-同舟云学术

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Station-keeping and formation flying based on nonlinear output regulation theory

Published:2018-12 Issue: Volume:153 Page:289-296
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Akiyama Yuki,Bando Mai,Hokamoto Shinji

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Contingency plans for the isee-3 libration-point mission;Dunham,1979

2. Transfer trajectory design for the soho libration-point mission;Dunham,1992

3. The Microwave Anisotropy Probe (Map) Mission, Vol. 29;Bennett,1997

4. Application of dynamical systems theory to trajectory design for a libration point mission;Barden;J. Astronaut. Sci.,1997

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2. On the dynamics and control of the Sun—Earth L2 tetrahedral formation;Astrodynamics;2021-11-12

3. An impulsive model predictive static programming based station-keeping guidance for quasi-halo orbits;Acta Astronautica;2021-11

4. Station-keeping of libration point orbits by means of projecting to the manifolds;Acta Astronautica;2019-10

5. Modeling relative motion of LEO satellites at different altitudes;Acta Astronautica;2019-03

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