通用惯导测试仿真系统的设计与实现  

Simulation and Verification Platform for General INS Test System

作　　者：禹亮[1] 程咏梅[1] 李军伟[1] 程承[1] 

机构地区：[1]西北工业大学,陕西西安710072

出　　处：《计算机仿真》2012年第8期93-96,100,共5页Computer Simulation

摘　　要：惯导性能测试一般在地面实验平台上进行,只能得到离散状态的测量结果,不能满足分析整个系统性能要求。建立飞行仿真系统能模拟各种飞行模态,并能够对惯导性能进行动态连续飞行轨迹下测试,在工程应用上具有重要意义。提出了惯导性能测试仿真系统的结构框架,并进行了系统功能分析与硬件设计,采用模块化设计思想,构造了基于控制律的飞控仿真模块及惯导反解算、通信等软件模块,给出了详细的设计及实现方法,并使用VC进行算法、系统实现。与惯导系统的联合仿真证明,为惯导测试系统的设计提供有效的平台。Architecture of the INS test simulation system was proposed, the functional analysis and the hardware design were also givem. According to the modular design thought, the software modules, such as the control law based flight simulation module, anti - solver module of INS and communication module, were constructed. The de- tailed design and realize method were shown. Tile VC tool was used to realize the algorithm and the system. The tic- bugging with the INS shows that the design is feasible.

关 键 词：惯导测试 动态连续 控制律 飞行控制仿真 

分 类 号：TP183[自动化与计算机技术—控制理论与控制工程]