Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance-Reference-Cited by-同舟云学术

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Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance

Published:1966 Issue: Volume: Page:209-246
ISSN:0079-6050
Container-title:Methods in Astrodynamics and Celestial Mechanics
language:
Short-container-title:

Author:

Lange Benjamin O.,Parkinson Bradford W.

Publisher

Elsevier

Reference36 articles.

1. “Inertial navigation,”;O'Donnell;J. Franklin Inst.,1958

2. Wrigley, W., Hovorka, J., and Woodbury, R., Inertial guidance, Institute of the Aeronautical Sciences, A Sherman M. Fairchild Publication Fund Paper FF-16 (January 1957).

3. Inertial Guidance;Draper,1960

4. Principles of Inertial Navigation;Savant,1961

5. Inertial Guidance;Pitman,1962

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1. Using the properties K-orthogonality for the transformation of the transition matrix between states of the spacecraft;XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2019

2. Optimal low-thrust rendezvous control.;AIAA Journal;1969-06

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