摘要
基于非线性系统高阶近似的思想，提出一种比推广卡尔曼滤波（ＥＫＦ）更接近非线性系统本质的近似滤波方法，并应用于飞行状态的参数估计（或称为飞行轨迹重构）问题。仿真和实际飞行数据计算结果表明：提出的非线性近似滤波方法比ＥＫＦ有更高的估计精度和更好的鲁棒性，对飞机机动形状、数据长度要求不高，滤波收敛速度快。利用飞行状态估计数学模型的具体特点，使计算量和存储量大幅度减少。该方法应用于非线性较强的飞行状态及参数估计问题。可得到比ＥＫＦ更好的结果。
new nonlinear approximate conditional mean filter is presented and applied to the flight state and parameter estimation of aircraft.The results of simulated and actual flight test data computations show that the new filter proposed here can give much more accurate estimates of flight state than extended Kalman filter(EKF)for different initial values and noise statistics.Moreover,the new method has fewer requirements for the maneuvering shapes,noise levels,data length and better convergency than that of EKF. The computational and storage requirements for one-step filtering updates of the new filter have been reduced greatly by exploiting some special features of system and measurement models and this makes it possible for the nonlinear filtering algorithm to be on-line realized on IBM-personal computer.It is proved that the new filter will be suitable for state and parameter of flight region at high angles of attack and can give good re-sults even for low sample rate flight test data.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第5期620-626,共7页
Acta Aeronautica et Astronautica Sinica
基金
国家自然科学基金
航空科学基金
关键词
非线性滤波
卡尔曼滤波器
飞行试验
nonlinear filters-approximation,Kalman filters,flight conditions-parameter identifi-cation,flight tests
