期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

抛弃传统方法——探索无尾战斗机的操纵技术 被引量：7

Lockheed Martin Has Picked ICF and Restore Programs for Tailless Fighters
原文传递
导出
摘要 美国国防部已经有越来越多的人对有人和无人驾驶的无尾布局战斗机表示出强烈的兴趣. Innovative Control Effector ( ICE ) and Reconfigurable Systems ( Restore ) have been two programs funded by US Air Force with Lockheed Martin Tactical Aircraft Systems a contractor. ICE program is developing several new contol effectors for tailless fighters and Restore program is developing a system that continuously measures and adapts contrrol gains to overcome battle damage and mechanical failure of tailless aircraft.
作者 余辉
出处 《国际航空》 1997年第2期46-48,共3页 International Aviation
关键词 战斗机 操纵技术 无尾式
分类号 V271.41 [航空宇航科学与技术—飞行器设计]
  • 相关文献

同被引文献51

  • 1余辉.美国掀起“无尾战斗机”研究热[J].国际航空,1996(10):18-21. 被引量：2
  • 2马超,李林,王立新.大展弦比飞翼布局飞机新型操纵面设计[J].北京航空航天大学学报,2007,33(2):149-153. 被引量：30
  • 3刘燕斌,陆宇平.非线性自适应控制在无尾飞控系统中的应用[J].航空学报,2006,27(5):903-907. 被引量：5
  • 4BOWLUS J A,MULTHOPP D,BANDA S S.Challenges and opportunities in tailless aircraft stability and control[R].AIAA 97-3830,1997.
  • 5MARTZ C W,CHURCH J D,GOSLEE J W.Free flight investigation to determine force and hinge moment characteristics at zero angle of attack of a 60°sweptback halfdelta tip control on a 60°swepthack delta wing at Mach numbers between 0.68 and 1.44[R].NACA RM L51114,1951.
  • 6Martz C W,Church J D.Flight investigation at subsonic,transonic,and supersonic velocities of the hinge moment characteristics,lateral control effectiveness,and wing damping in roll of a 60°sweptback delta wing with half delta tip ailerons[R].NACA RM L51G18,1951.
  • 7William J G.Innovative control effectors (configuration 101) dynamic wind tunnel test report rotary balance and force oscillation tests[R].AFRL-VA-WP-TP-1998-3043,1998.
  • 8YOUNG V S.Science and technology opportunities for unmanned aerial vehicles[A].The 3rd US-European Competition and Workshop on Micro Air Vehicles & the 7th European Micro Air vehicle Conference and Flight Competition[C].2007,in Toulouse,France.
  • 9Gillard W J,Dorsett K M.Directional control for tailless aircraft using all moving wing tips[R].AIAA-97-3487.1997.
  • 10BOWLUS J A, MULTHOPP D and BANDA S S. Challenges and opportunities in tailless aircraft stability and control[R]. AIAA 97-3830, 1997.

引证文献7

二级引证文献71

国际航空
1997年 第2期

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部