探测与控制学报
探測與控製學報
탐측여공제학보
JOURNAL OF DETECTION & CONTROL
2014年
6期
57-62
,共6页
GPS/INS紧组合导航%容积卡尔曼滤波%强跟踪滤波%均方根策略%导航精度
GPS/INS緊組閤導航%容積卡爾曼濾波%彊跟蹤濾波%均方根策略%導航精度
GPS/INS긴조합도항%용적잡이만려파%강근종려파%균방근책략%도항정도
GPS/INS tightly integrated navigation%cubature Kalman filter%strong tracking filter%square-root%navigation accuracy
针对 GPS/INS(Global Positioning System/Inertial Navigation System)紧组合导航系统在卫星信号缺失情况下导航精度降低,容积卡尔曼滤波(Cubature Kalman Filter ,CKF)应用中存在模型误差和计算误差的问题,提出了适用于该背景下的强跟踪均方根容积卡尔曼滤波(Square-Root CKF)算法。该算法通过人为地相对突出滤波过程中新数据的作用,提高了算法在模型不确定时的鲁棒性;均方根策略保证了协方差阵的正定性和对称性。仿真实验表明,改进的算法能够提高导航精度,在卫星信号缺失情况下其效能发挥地更好,提高了组合导航适应复杂环境的能力。
針對 GPS/INS(Global Positioning System/Inertial Navigation System)緊組閤導航繫統在衛星信號缺失情況下導航精度降低,容積卡爾曼濾波(Cubature Kalman Filter ,CKF)應用中存在模型誤差和計算誤差的問題,提齣瞭適用于該揹景下的彊跟蹤均方根容積卡爾曼濾波(Square-Root CKF)算法。該算法通過人為地相對突齣濾波過程中新數據的作用,提高瞭算法在模型不確定時的魯棒性;均方根策略保證瞭協方差陣的正定性和對稱性。倣真實驗錶明,改進的算法能夠提高導航精度,在衛星信號缺失情況下其效能髮揮地更好,提高瞭組閤導航適應複雜環境的能力。
침대 GPS/INS(Global Positioning System/Inertial Navigation System)긴조합도항계통재위성신호결실정황하도항정도강저,용적잡이만려파(Cubature Kalman Filter ,CKF)응용중존재모형오차화계산오차적문제,제출료괄용우해배경하적강근종균방근용적잡이만려파(Square-Root CKF)산법。해산법통과인위지상대돌출려파과정중신수거적작용,제고료산법재모형불학정시적로봉성;균방근책략보증료협방차진적정정성화대칭성。방진실험표명,개진적산법능구제고도항정도,재위성신호결실정황하기효능발휘지경호,제고료조합도항괄응복잡배경적능력。
Aiming at the problems that the navigation accuracy of GPS/INS tightly integrated navigation was lowered under condition of GPS signal invalidation,model error and calculation error existing in the application of CKF,a strong tracking SRCKF was presented under the background.By stressing the function of new data artificially,this al-gorithm improved the robustness when the model was uncertain,and the square-root strategy ensured the positive defi-niteness and symmetry of covariance matrix.Simulation results showed that the improved algorithm could improve the navigation accuracy and had better efficiency under the condition of GPS signal invalidation.