Work

Spacecraft Trajectory Optimization Based on Discrete Sets of Pseudoimpulses

Year: 2009

Type: article

Source: Journal of Guidance Control and Dynamics

DOI: 10.2514/1.41201

Author: Yuri Ulybyshev

Institution: S. P. Korolev Rocket and Space Corporation Energia (Russia)

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W1990225020

FWCI: 4.678

Cites: 30

Cited by: 21

Related to: 10