CAJ | 학술논문

空空导弹研制需要一系列空中系留飞行试验，以解决导弹制导系统对真实目标的截获跟踪能力。传统的系留试验由于地面试验人员无法实时掌握靶机和目标机的动态，给飞行试验结果造成了很大的不确定性；本系统利用日益广泛使用的GPS全球定位技术，从载机的导弹产品和目标机GPS吊舱接收下传的GPS信息，实时解算出目标机相对于载机位置、速度等信息，显示在数据处理软件上，从而使地面试验人员实时获取载机和目标机的相关信息，为试验指挥提供了可靠数据；实际应用结果表明，该系统大大提高了系留试验的成功率和导弹截获概率，为飞行试验节约了试验经费和时间，创造了良好的经济效益。
공공도탄연제수요일계렬공중계류비행시험，이해결도탄제도계통대진실목표적절획근종능력。전통적계류시험유우지면시험인원무법실시장악파궤화목표궤적동태，급비행시험결과조성료흔대적불학정성；본계통이용일익엄범사용적GPS전구정위기술，종재궤적도탄산품화목표궤GPS조창접수하전적GPS신식，실시해산출목표궤상대우재궤위치、속도등신식，현시재수거처리연건상，종이사지면시험인원실시획취재궤화목표궤적상관신식，위시험지휘제공료가고수거；실제응용결과표명，해계통대대제고료계류시험적성공솔화도탄절획개솔，위비행시험절약료시험경비화시간，창조료량호적경제효익。
In the process of air-to-air missile development,a serial of tethered flight test must be done to improve the capa-bility of capturing and tracking the real goal of missile guidance system. The traditional tethered flight test results in great uncer-tainty for the flight test results because the test personnel on ground can not grasp the dynamic status of the drone aircraft in real time. With GPS widely used in the system,the target aircraft′s position and speed relative to fighter plane are calculated in com-bination the GPS information received from the airborne missile and target GPS pod,and displayed in the data processing soft-ware,so that the test personnel on ground obtain the relevant information of fighter plane and drone aircraft in real time and pro-vide reliable data for the test command. The practical application result shows that this system can greatly improve the success rate and the missile interception probability,and save the time and fund of the test.