Work

Trigonometric-Type Sliding Mode Attitude Control for Rigid Spacecraft with Arbitrary Convergence Time

Year: 2025

Type: conference-paper

Source: Conference on Fully Actuated System Theory and Applications (FASTA)

DOI: 10.1109/fasta65681.2025.11138905

Authors: Yu-Tian Xu, Ai-Guo Wu

Institution: Harbin Institute of Technology

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G7459089890

OpenAlex ID: W4414170689

FWCI:

Cites: 14

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