Work

Combined-Cycle Propulsion-Involved Trajectory Optimization and Performance-Driven Attitude Control for Aerospace Plane During the Ascent Phase

Year: 2024

Type: article

Source: IEEE Transactions on Intelligent Transportation Systems

DOI: 10.1109/tits.2024.3470528

Authors: Jianguo Guo, Lecheng Liang, Zongyi Guo

Institution: Northwestern Polytechnical University

Language: English

Topic: Guidance and Control Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, Fundamental Research Funds for the Central Universities

Awards: G3529242898, G4701702971, G958898749

OpenAlex ID: W4403277144

FWCI: 2.493

Cites: 34

Cited by: 14

Related to: 10