Description of 4 Spacecraft, Moving on Elliptic Kepler Orbits
Vladimir P. Zhukov, Nikolai K. Iakovlev, Alexander A. Bochkarev, Nikita E. Logvinenko, Sergei M. Kurchev, Vlas A. Karavaikin, Ivan A. Radko

TL;DR
This paper introduces a new analytical approach for describing a four-spacecraft formation on elliptical Kepler orbits, enabling precise measurement of gravitational field gradients and simplifying mission planning.
Contribution
It presents an analytical solution for spacecraft formation motion using Cartesian coordinates of a chief spacecraft, with a focus on volume polynomial properties and mission planning simplifications.
Findings
Analytical solutions use Cartesian coordinates of the chief spacecraft.
Volume of the tetrahedron is a polynomial of degree 3 or 2, depending on orbit synchronization.
Method simplifies mission planning for interplanetary gravitational measurements.
Abstract
The four-spacecraft formation is essential for measurements of various physical fields. The use of this formation on substantially elliptical heliocentric Kepler orbits allows measuring gradients of gravitation field in Solar system. The accuracy of the measurements will be sufficient to confirm or to refute modified theories of gravity. In this paper a new approach for the description of this formation is presented. The analytical solutions of the linearized motion equations are obtained. The distinctive feature of the solutions is that they use Cartesian coordinates of one of the spacecraft, termed the chief. These solutions have a clear physical meaning. It is shown, that the volume of a tetrahedron formed by spacecraft is a polynomial of 3-rd degree of Cartesian coordinates of the chief. The polynomial's coefficients are functions of initial spacecraft coordinates and velocities and…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Field-Flow Fractionation Techniques · Space Satellite Systems and Control
