Constrained input-to-state controller design for spacecraft attitude stabilization

Mingxiang Li, Mingshan Hou, Chunwu Yin. Constrained input-to-state controller design for spacecraft attitude stabilization. In 2016 American Control Conference, ACC 2016, Boston, MA, USA, July 6-8, 2016. pages 5862-5866, IEEE, 2016. [doi]

Abstract

Abstract is missing.