Work

Adaptive weighted robust control for flexible launch vehicles based on rigid-elastic coupling analysis

Year: 2026

Type: article

Source: Aerospace Science and Technology

DOI: 10.1016/j.ast.2026.113579

Authors: Xingyu Jiang, Peng Shi, Shengping Gong

Institution: Beihang University

Language: English

Topic: Aeroelasticity and Vibration Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

Funder: National Natural Science Foundation of China

Award: G198608382

OpenAlex ID: W7167624192

FWCI:

Cites: 62

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Related to: 10