Work

New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit

Year: 2002

Type: article

Source: Journal of Guidance Control and Dynamics

DOI: 10.2514/2.4875

Authors: Koji Yamanaka, Finn Ankersen

Institution: European Space Research and Technology Centre

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2131283498

FWCI: 8.42

Cites: 7

Cited by: 601

Related to: 10