Work

Optimal impact angle guidance law based on collision geometry for axially maneuvering targets

Year: 2025

Type: article

Source: Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

DOI: 10.1177/09544100251401024

Authors: Jiedong He, Meng Yu, Yin Wang

Institution: Nanjing University of Aeronautics and Astronautics

Language: English

Topic: Guidance and Control Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G6461297872

OpenAlex ID: W4416695459

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Cites: 30

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