2015Microgravity Science and TechnologyRequires access

How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

A. V. Sedelnikov, K. I. Potienko

Open publisher page 18 citations

Abstract

This record does not include an abstract. Use the full-text link above if available.

About this research paper

What this paper is about

An abstract is not available in the OpenAlex record for this paper.

Why it matters

OpenAlex reports 18 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Key concepts: Elliptic orbit, Spacecraft, Orbit determination, Orbit (dynamics), Aerospace engineering, Physics, Geodesy, Computer science

Related papers

Back to paper searchBrowse research topicsOriginal source
How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit — Research Paper | ScholarLens