摘要
飞行轨迹动态参数是验证捷联惯导系统、组合导航系统等算法有效性的重要依据。利用飞行控制原理设计了一种通用的飞机飞行仿真轨迹,并在Visual Studio 2005开发环境下设计了飞行轨迹仿真软件。该仿真软件产生的数据有效地测试了某型导航系统导航参数的误差精度,验证了捷联惯导算法的正确性。
The dynamic parameters of the flight track are important basis what are used to verify the effective- ness of the algorithm of the strapdown inertial navigation system or the integrated navigation system. Using the flight control principle, a general flight simulation track and its generation software on Visual Studio 2005 de- veloping platform are designed. The error precision of the navigation parameters and the correctness of the algo- rithm are tested by the generated data of the simulation software.
出处
《测控技术》
CSCD
北大核心
2013年第5期138-142,共5页
Measurement & Control Technology
关键词
动态参数
导航系统
飞行轨迹仿真软件
误差精度
dynamic parameter
navigation system
flight track simulation software
error precision
