Work

Finite-time convergent control for spacecraft attitude stabilization based on the adding power integrator technique

Year: 2024

Type: article

Source: Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

DOI: 10.1177/09544100241286237

Authors: Boyan Jiang, Yingchen Feng, Qiuhan Su, Xiaoyong Huang, Chuanjiang Li

Institutions: Changzhou Institute of Technology, Hohai University, Harbin Institute of Technology

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, Basic Research Program of Jiangsu Province

Awards: G6429293251, G8895800156

OpenAlex ID: W4402700290

FWCI: 0.89

Cites: 46

Cited by: 5

Related to: 10