兵工自动化
兵工自動化
병공자동화
Ordnance Industry Automation
2015年
10期
31-34
,共4页
无人机%火箭助推器%模型%能量%仿真
無人機%火箭助推器%模型%能量%倣真
무인궤%화전조추기%모형%능량%방진
UAV (unmanned aerial vehicle)%RATO (rocket-assisted takeoff)%model%energy%simulation
为节省研发过程中的成本和时间,提出一种基于商用货架产品(commercial-off-the-shelf,COTS)的无人机火箭助推起飞设计思路.通过分析无人机火箭发射过程和要求,立足现有火箭助推器定型产品,进行发射参数估算,完成了火箭助推器的选型,在此基础上进行火箭助推发射建模、方案设计、仿真分析.仿真结果表明:该方法能确立火箭助推起飞最优发射角和安装角,可实现该型无人机的稳定安全发射,对其他同类无人机火箭助推起飞系统的设计也有很好的工程借鉴经验.
為節省研髮過程中的成本和時間,提齣一種基于商用貨架產品(commercial-off-the-shelf,COTS)的無人機火箭助推起飛設計思路.通過分析無人機火箭髮射過程和要求,立足現有火箭助推器定型產品,進行髮射參數估算,完成瞭火箭助推器的選型,在此基礎上進行火箭助推髮射建模、方案設計、倣真分析.倣真結果錶明:該方法能確立火箭助推起飛最優髮射角和安裝角,可實現該型無人機的穩定安全髮射,對其他同類無人機火箭助推起飛繫統的設計也有很好的工程藉鑒經驗.
위절성연발과정중적성본화시간,제출일충기우상용화가산품(commercial-off-the-shelf,COTS)적무인궤화전조추기비설계사로.통과분석무인궤화전발사과정화요구,립족현유화전조추기정형산품,진행발사삼수고산,완성료화전조추기적선형,재차기출상진행화전조추발사건모、방안설계、방진분석.방진결과표명:해방법능학립화전조추기비최우발사각화안장각,가실현해형무인궤적은정안전발사,대기타동류무인궤화전조추기비계통적설계야유흔호적공정차감경험.
In order to save the cost and time in the development process, provides a new way of the rocket-assisted take-off (RATO) for UAV base on commercial-off-the-shelf (COTS). Through analyzing the demand and process of launch, the launch parameters are estimated and the RATO selected, on the basis of existing case-hardened RATO. Then, modeling the launch, plan the project, simulation and analysis. As a result, a way of the optimum angle and fixing for launch is given. It can realize safe and stable launch of the UAV. Similarly, this is good use for reference to plan the other lunch system of the congeneric UAV in engineering.
