Spacecraft Transfer Optimization with Releasing the Additional Fuel Tank and the Booster to the Earth Atmosphere.

Autor:	Grigoriev, I. S., Proskuryakov, A. I.
Předmět:	FUEL tanks ORBITS of artificial satellites SPACE debris NEWTON-Raphson method ORBITAL transfer (Space flight) SPACE vehicles
Zdroj:	Automation & Remote Control; Mar2023, Vol. 84 Issue 3, p211-225, 15p
Abstrakt:	This paper considers the idea of reducing the debris of near-Earth space by releasing the spent parts of a spacecraft on orbits touching the conditional boundary of the Earth's atmosphere. We optimize the spacecraft transfer trajectory from a circular reference orbit of an artificial Earth satellite to a target elliptical orbit in a modified pulse problem statement. The convergence of Newton's method is improved by introducing a series of auxiliary coordinate systems at each point of applying an impulse action. The derivatives in the transversality conditions are calculated using a special numerical-analytical differentiation technique. [ABSTRACT FROM AUTHOR]
Databáze:	Complementary Index
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