State interpolation for on-board navigation systems-Reference-Cited by-同舟云学术

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State interpolation for on-board navigation systems

Published:2001-03 Issue:3 Volume:5 Page:209-220
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Montenbruck Oliver,Gill Eberhard

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. General characteristics of real-time on-board orbit determination;Berthias,1997

2. Iss. 2D, Daimler-Chrysler Aerospace; CH-IT-DID-0001, 1998/10/26,1998

3. A family of embedded Runge–Kutta formulae;Dormand;J. Comput. Appl. Math.,1980

4. Runge–Kutta triples;Dormand;Comput. Math. Appl.,1986

5. Interpolants for Runge–Kutta formulas;Enright;ACM T. Math. Software,1986

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1. A Novel Navigation Approach of Low Earth Orbit Satellites Formation Based on Reduced Relative Orbital Elements;Lecture Notes in Electrical Engineering;2021-10-30

2. A long‐term broadcast ephemeris model for extended operation of GNSS satellites;NAVIGATION;2020-12-28

3. Orbit Design of Spacecraft on Elliptical Orbit;Navigation: Science and Technology;2018-08-15

4. Numerical Integration of the Equations of Motion;Practical Astrodynamics;2017-11-28

5. Space Applications;Springer Handbook of Global Navigation Satellite Systems;2017

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