Work

Exponential Tracking Control of Spacecraft Attitude Dynamics: Explicit Relationship Between Convergence Rate and Input Constraints

Year: 2026

Type: article

Source: International Journal of Robust and Nonlinear Control

DOI: 10.1002/rnc.70465

Authors: Haichao Zhang, Bing Xiao, Jingwen Xu, Huijun Li

Institutions: Sichuan Police College, Northwestern Polytechnical University

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Major Science and Technology Projects of China

Award: G1741168638

OpenAlex ID: W7134192015

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Cites: 42

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