摘要
临近空间飞艇在发放前通常停放在艇库内,一旦离开艇库就不可避免地受到艇库外天气,尤其地面风的影响,不仅影响飞艇发放操作的快捷和安全,而且还事关飞行试验的成败。文章建立了大型飞艇在地面受两侧约束时的力学模型,采用动力学方法,分析了受到地面风作用时飞艇的姿态和约束拉力的变化,得到地面风起时和风速稳定后的解析解,评估了飞艇受到地面风作用时的稳定性和安全性。通过分析得到在两侧约束条件下飞艇对正向风和侧风的承受极限,为临近空间飞艇采用两侧约束方式的可行性提供了判据,也为今后发展临近空间飞艇发放技术提供借鉴。
Typically, the near space airship parks in the hangar before launch. As soon as near space airship leaves its hangar it will be affected by the weather and particularly by the wind, which not only affect the rapidity and security of the airship operation, but also relate to the success of the flight test. A mechanical model was established when an airship was outside its hangar with both sides restricted. The variations of airship yaw and rope tension were analyzed by using dynamic method. The analytical solution was obtained at the beginning and stable state of the wind, then, the stability and safety of an airship were also evaluated. The ultimate bearings of forward wind and crosswind on an airship outside the hangar were proposed. The result quantifies the indicators of meteorological conditions, and provides references of scientific and rational methods for the launch technology of near space airship in the future.
作者
张泰华
姜鲁华
张冬辉
王立祥
ZHANG Taihua JIANG Luhua ZHANG Donghui WANG Lixiang(Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing 100094, China University of Chinese Academy of Science, Beijing 100049, China 3. Institute of High Energy Physics, Chinese Academy of Sciences, Beijing 100049, China)
出处
《中国空间科学技术》
EI
CSCD
北大核心
2016年第5期72-80,共9页
Chinese Space Science and Technology
基金
高分辨率对地观测系统重大专项(飞艇总体技术研究与试验)
中科院知识创新重大项目(平流层试验飞艇研制与集成演示)
关键词
临近空间飞艇
高空长航时演示验证飞艇
约束力
稳定性分析
发放技术
near space airship
high altitude long endurance-demonstrator
force of constraint
stability analysis
launch technology