摘要
给出了基于线性矩阵不等式(LMI)的鲁棒H∞状态估计器的设计过程。该方法克服了基于代数Riccati方程(ARE)中处理不确定性的限制,整个设计过程完全通过求解三个LMI得到,简化了设计过程。在惯性导航系统(INS)地面自对准中的应用表明,基于LMI的鲁棒H∞状态估计器在系统具有不确定性时,仍然能使估计误差保持收敛,优于传统的性能状态估计。
The design approach to robust H ∞ state estimator for linear systems with energy bounded exogenous noise inputs and structural uncertainties solved via three linear matrix inequalities(LMIs) is presented. This approach is better than conventional one based on algebraic Riccati equations(AREs) while dealing with the uncertainties of systems. The application of the design technique of robust H ∞ state estimation in inertial navigation systems (INS) ground alignment shows that robust H ∞ state estimation based on LMIs has more optimal performance than conventional H 2 estimator.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
1998年第6期646-651,共6页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
鲁棒控制
估计量
惯性导航
线性矩阵不等式
robust controls
estimators
nertial navigation
linear matrix inequalities (LMIs)