This research was supported by the National Natural Science Foundation of China under Grant No.61903312;Huiyan Project for Research on Innovation and Application of Space Science and Technology under Grant No.CD2B65B6.
In this paper,a fully-actuated system approach(FASA)based control method is proposed for rigid spacecraft attitude tracking with actuator saturation.First,a second-order fully-actuated form of spacecraft attitude erro...
supported by the Natural Science Foundation of China under Grant Nos.61374090,and 61473171;the Program for Scientific Research Innovation Team in Colleges and Universities of Shandong Province;the Taishan Scholarship Project of Shandong Province
This paper is concerned with control and optimization for a sampled-data system with quantization and actuator saturation. Based quantization and actuator saturation a controller is introduced. The corresponding close...
This research is supported by the National Nature Science Foundation of China under Grant Nos. 60774009, 61074068, 61034007, the Research Fund the Doctoral Program of Chinese Higher Education under Grant No. G200804220028, the Independent Innovation Foundation of Shandong University under Grant No. 2010TS078, and the Nature Science Foundation of Shandong Province under Grant No. ZR2010FM013.
This paper investigates parallel simultaneous stabilization (PSS) of a set of multi-input nonlinear Port-Controlled Hamiltonian (PCH) systems subject to actuator saturation (AS), and proposes a number of results...
Low gain feedback refers to certain families of stabilizing state feedback gains that are pararaeterized in a scalar and go to zero as the scalar decreases to zero. Low gain feedback was initially proposed to achieve ...