Work

Exponential Attitude Tracking and Vibration Control for 3-D Flexible Spacecraft With Disturbances and Quantized Inputs

Year: 2025

Type: article

Source: IEEE Transactions on Automation Science and Engineering

DOI: 10.1109/tase.2025.3591968

Authors: Le Li, Zhongkui Li

Institutions: Peking University, State Key Laboratory of Turbulence and Complex Systems

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, China Postdoctoral Science Foundation

Awards: G1276146209, G2110336733, G4606779385, G5455908029, G8670534201, G8993889159

OpenAlex ID: W4412610029

FWCI: 1.998

Cites: 40

Cited by: 5

Related to: 10