点击次数：
所属单位：北京航空航天大学
发表刊物：PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGIN
项目来源：北京市科技重点项目
关键字：Small rotary-wing unmanned aircraft, disturbance observer control, feedback control
摘要：As a complex system, control performance of small rotary-wing unmanned aircraft is easily affected by measurement errors and environment disturbances. This paper proposes a nonlinear disturbance observer-based control to improve control performance. The constant and harmonic disturbance that is generated by the exogenous system with modeling perturbation can be estimated and rejected effectively. The random disturbance with certain bound can be reduced by the feedback control. By solving linear matrix inequality, the parameters for feedback control and nonlinear disturbance observer can be sel
合写作者： Fang,Liu, Pei,Lu, Xusheng,Lei
论文类型：基础研究
文献类型：期刊
是否译文：否
发表时间：2013-11-21
发布期刊链接：http://journals.sagepub.com/doi/abs/10.1177/0954410013513414