Work

Constrained Fuel- and Time-Optimal Six-Degree-of-Freedom Powered Descent Guidance Using Indirect Optimization

Year: 2025

Type: article

Source: Journal of Spacecraft and Rockets

DOI: 10.2514/1.a36497

Authors: Nicholas P. Nurre, Ehsan Taheri

Institution: Auburn University

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4417536765

FWCI: 0.782

Cites: 50

Cited by: 2

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