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为了提高飞行控制软件的模块化、可测试性和可维护性,提出一种通用化无人直升机飞行控制软件框架设计方法。通过分析飞行控制软件的功能和性能需求,构建了主要包括输入/输出模块、飞行管理模块和飞行控制模块的软件框架,重点分析了软件框架的主要结构以及各个模块的功能,并验证了软件的功能和性能。实际仿真测试结果表明,该软件的功能完整且性能满足使用要求。
In order to improve the modularization, testability and maintainability of flight control software, a universal design method of unmanned helicopter flight control software framework is proposed. By analyzing the function and performance requirements of flight control software, a software framework including I / O module, flight management module and flight control module is constructed. The main structure of software framework and the function of each module are analyzed emphatically. The software Function and performance. The actual simulation test results show that the software features complete and performance to meet the requirements.