CAJ | 학술논문

为保证地磁导航对飞行器快速反应的要求，采用了基于飞行器缩比模型的磁干扰补偿模型参数求解方法。首先，分析了飞行器磁干扰补偿模型以及小信号模型的求解方法；然后，采用飞行器缩比模型代替飞行器进行地面试验，并在地面快速求解飞行器载体磁干扰补偿模型参数；最后，通过分析试验结果及其补偿效果，验证了补偿模型求解算法的良好磁环境适应性以及该试验方案的实际可行性。
위보증지자도항대비행기쾌속반응적요구，채용료기우비행기축비모형적자간우보상모형삼수구해방법。수선，분석료비행기자간우보상모형이급소신호모형적구해방법；연후，채용비행기축비모형대체비행기진행지면시험，병재지면쾌속구해비행기재체자간우보상모형삼수；최후，통과분석시험결과급기보상효과，험증료보상모형구해산법적량호자배경괄응성이급해시험방안적실제가행성。
In order to ensure the rapid response of geomagnetic navigation to aircraft ,the method is used to solve the parameters of the magnetic disturbance compensation model based on the aircraft scale model .Firstly ,an analysis is made of solving method for the aircraft magnetic disturbance com-pensation model and small-signal model .Then ,the aircraft scale model is used instead of aircraft for ground tests to obtain the parameters of the magnetic interference compensation model of aircraft car-rier through fast solution .Finally ,the test results and compensation effect w hich have been analyzed verify the good environmental adaptability of the compensation model algorithm and the magnetic practical feasibility of the ground tests .