武装直升机空战关键技术问题研究 |
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引用本文: | 曾国贵,姜长生.武装直升机空战关键技术问题研究[J].直升机技术,2002(3):29-32. |
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作者姓名: | 曾国贵 姜长生 |
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作者单位: | 1. 中国直升机设计研究所,景德镇,333001 2. 南京航空航天大学,南京,210016 |
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摘 要: | 本文论述了武装直升机空战的几个关键技术问题。首先建立了简化的武装直升机空战动力学和运动学模型,阐明了模型简化的具体方法;其次给出了直升机空战的结构图,并分析了空战的基本原理,同时简述了空战机动策略的选取原则,描述了直升机空战的基本特征;最后系统地说明了直升机空战中的航路规划技术,并提出了未来旋翼机的设想。
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关 键 词: | 武装直升机 空战 机动策略 空战特征 航路规划 |
RESEARCH OF KEY TECHNICAL PROBLEMS ABOUT ATTACK HELICOPTER AIR-COMBAT |
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Authors: | ZENG Guo-gui JIANG Chang-sheng |
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Abstract: | This paper treats the several key technical problems on attack helicopter air-combat. First, the simplified dynamics and kinematics model of attack helicopter air-combat are created,and the specific method on simplification of the model is given. Second, the constructional drawing on helicopter air-combat is shown, the basic theory of helicopter air-combat is introduced,at the same time,the principle that the strategy of helicopter air-combat maneuver is chosen is analyzed and the paper describes the feature of helicopter air-combat. In the end, the paper shows the helicopter air-combat trajectory programming technology, and indicates the imagine of future rotaplane. |
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Keywords: | attack helicopter air-combat maneuverable strategy air-combat feature trajectory programming |
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