| 战斗机滚转姿态快速性研究 |
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| 引用本文： | 程才凤,尹江辉,刘昶.战斗机滚转姿态快速性研究[J].飞行力学,2003,21(2):13-15,19. |
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| 作者姓名： | 程才凤 尹江辉 刘昶 |
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| 作者单位： | 南京航空航天大学,空气动力学系,江苏,南京,210016 |
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| 摘 要： | 介绍了战斗机中等幅度滚转姿态快速性的定义，应用欧拉法对19种飞机构形的滚转快速性进行了仿真计算．其结果与地面模拟战斗机攻击机动试验相比较，表明滚转姿态快速性与滚转模态时间常数、滚转操纵效能、副翼操纵速率和控制系统增益等飞行品质要求密切相关，飞行品质标准MIL—STD—1797没有完全涵盖中等幅度滚转姿态变化的要求。
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| 关 键 词： | 战斗机 滚转姿态快速性 飞行品质 滚转操纵效能 |
| 文章编号： | 1002-0853(2003)02-0013-03 |
Research on Roll Attitude Quickness Criteria for Fighter |
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| CHENG Cai feng,YIN Jiang hui,LIU Chang.Research on Roll Attitude Quickness Criteria for Fighter[J].Flight Dynamics,2003,21(2):13-15,19. |
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| Authors: | CHENG Cai feng YIN Jiang hui LIU Chang |
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| Abstract: | Based on the definition of moderate amplitude roll attitude quickness criteria for fighter, the roll attitude quickness is calculated by the Euler method for 19 types aircraft configurations in this paper. The results of the simulation calculation are compared with the pilots simulation tests on aggressive maneuvering in roll. The conclusions are obtained that roll attitude quickness is closely related to the flying qualities, such as roll mode time constant, roll control sensitivity, aileron control effectiveness and control system augment. Requirements for moderate amplitude maneuvering roll attitude changes are not completely involved in MIL STD 1797A. |
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| Keywords: | fighter roll attitude quickness flying qualities |
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