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基于航线数据库的自适应导航系统
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作者 麻士东 张威 《华北航天工业学院学报》 2003年第3期22-25,共4页
飞行的导航与制导是保障飞行任务的重要条件。文章分析了基于航线数据库的导航制导系统,介绍了指令式的制导方式,即自适应的制导系统,它是首先测量飞机的运行状态,并将数据传给存有航路数据的计算机,经比较后,得出飞机飞行与预定航线的... 飞行的导航与制导是保障飞行任务的重要条件。文章分析了基于航线数据库的导航制导系统,介绍了指令式的制导方式,即自适应的制导系统,它是首先测量飞机的运行状态,并将数据传给存有航路数据的计算机,经比较后,得出飞机飞行与预定航线的偏差,从而得出控制舵面运动的指令,将指令传到飞机舵面,飞机自动控制调整航向及姿态。 展开更多
关键词 飞机 航线数据库 自适应导航系统 数学模型 自适应控制器
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自适应战术导航系统
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作者 魏艳 《导航》 2007年第1期64-70,共7页
自适应战术导航系统(AdaptiveTacticalNavigation(ATN))是美国怀特·帕特森空军基地(Wright—PattersonAFB)怀特研究实验室的航空部自1986年至1990年在一个计算机模拟环境中设计、研发和论证的项目。ATN系统是基于知识系统的... 自适应战术导航系统(AdaptiveTacticalNavigation(ATN))是美国怀特·帕特森空军基地(Wright—PattersonAFB)怀特研究实验室的航空部自1986年至1990年在一个计算机模拟环境中设计、研发和论证的项目。ATN系统是基于知识系统的一个实验室样机。结合了人工智能(AI)技术和先进的导航算法,可以对20世纪90年代的战术飞机实现导航系统管理和决策辅助。ATN系统的设计目的就是管理未来多传感器导航组,根据任务目标、任务阶段、威胁环境、设备健康状况、设备可用性、战斗损伤等等动态地选择使用最佳的导航信息源。 展开更多
关键词 自适应战术导航系统 基本导航系统 专家导航系统 导航源管理器
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Application of Adaptive Kalman Filtering Algorithm in IMU/GPS Integrated Navigation System 被引量:13
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作者 GAO Weiguang YANG Yuanxi CUI Xianqiang ZHANG Shuangcheng 《Geo-Spatial Information Science》 2007年第1期22-26,共5页
The IMU(inertial measurement unit) error equations in the earth fixed coordinates are introduced firstly. A fading Kalman filtering is simply introduced and its shortcomings are analyzed, then an adaptive filtering ... The IMU(inertial measurement unit) error equations in the earth fixed coordinates are introduced firstly. A fading Kalman filtering is simply introduced and its shortcomings are analyzed, then an adaptive filtering is applied in IMU/GPS integrated navigation system, in which the adaptive factor is replaced by the fading factor. A practical example is given. The resuits prove that the adaptive filter combined with the fading factor is valid and reliable when applied in IMU/GPS integrated navigation system. 展开更多
关键词 integrated navigation adaptive filtering fading filtering the earth fixed coordinates
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Application of Adaptive Divided Difference Filter on GPS/IMU Integrated Navigation System
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作者 ZHAO Pei-pei LI Shi-xin XIAO Zhi-tao 《Semiconductor Photonics and Technology》 CAS 2009年第3期158-162,178,共6页
The efficient and accurate approximate nonlinear filters have been widely used in the estimation of states and parameters of dynamical systems. In this paper, an adaptive divided difference filter is designed for prec... The efficient and accurate approximate nonlinear filters have been widely used in the estimation of states and parameters of dynamical systems. In this paper, an adaptive divided difference filter is designed for precise estimation of states and parameters of micromechanical gyro navigation system. Based on the investigation of nonlinear divided difference filter the adaptive divided difference filter(ADDF) was designed, which takes account of the incorrect time-varying noise statistics of dynamical systems and compensation of the nonlinearity effects neglected by linearization. And its performance is superior to that of DDF and extended Kalman filter(EKF). Simulation results indicate that the advantages of the proposed nonlinear filters make them attractive alternatives to the extended Kalman filter. 展开更多
关键词 ADAPTIVE divided difference filter noise estimation
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