Barrier function-based adaptive integral sliding mode finite-time attitude control for rigid spacecraft

Author:

Wang JieORCID,Hu Yushang,Ji Wenqiang

Funder

National Natural Science Foundation of China

the Key R &D Program of Hebei Province

Natural Science Foundation of Hebei Province

Postdoctoral Research Foundation of China

Science and Technology Research Project of Colleges and Universities in Hebei Province

Undergraduate Education and Teaching Reform Research and Practice Project

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

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