Aeronautics and Human-Engineering Joint Research to Avoid Aircraft Stall Accidents
航空学和人体工程联合研究以避免飞机失速事故
基本信息
- 批准号:10305072
- 负责人:
- 金额:$ 25.66万
- 依托单位:
- 依托单位国家:日本
- 项目类别:Grant-in-Aid for Scientific Research (A)
- 财政年份:1998
- 资助国家:日本
- 起止时间:1998 至 2001
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
When the wing angle of attack of the aircraft is increased, sudden decrease of lift happens at certain angle of attack. This is called a wing stall and is known as a cause of the aircraft accident. To avoid the aircraft stall accidents, it is necessary to consider not only the flight dynamical aspects of aircrafts but also the human engineering aspects of pilots. The purpose of this research is to make clear the stall avoidance and recovery techniques by the pilot from the points both of flight dynamics and of human engineering. Aerodynamic and flight dynamic stall characteristics, piloting technique and the pilot workload have been studied in this research.First, pilot workload measurements using a flight simulator have been done to investigate pilot skills and the pilot workload. A pilot workload evaluation method has been established that mainly concentrates on the pilot's information processing. Results showed that the workload of the in-experienced pilot is continuously high dining the whole flight. High workload precludes the accurate and correct decision making that increases the workload further.Second, flight tests have been conducted using the actual aircraft to measure the pilot eye movements during the flight including when the aircraft experiences the stall. Results indicated that the proper piloting and accurate decision by the pilot are necessary to maintain the aircraft attitude correctly, even when the aircraft experiences the stall. Importance of eye scanning onto the proper instruments was also discussed.Finally, flight dynamical characteristics when the aircraft experiences the stall have been investigated to predict the aircraft stall characteristics.
当飞机的机翼迎角增大时,在某一迎角处升力会突然下降。这被称为机翼失速,是飞机事故的一个原因。为了避免飞机失速事故的发生,不仅要考虑飞机的飞行动力学因素,而且要考虑飞行员的人体工程学因素。本研究的目的是从飞行力学和人机工程学的角度来阐明飞行员的失速避免和改出技术。本研究主要针对气动与飞行动态失速特性、驾驶技术与驾驶员工作负荷进行研究。首先,利用飞行模拟器进行驾驶员工作负荷量测,以了解驾驶员的驾驶技术与驾驶员工作负荷。建立了一种以飞行员信息处理为主要内容的飞行员工作负荷评估方法。结果表明,经验不足的飞行员在整个飞行过程中的工作负荷一直很高。高工作量阻碍了准确和正确的决策,从而进一步增加了工作量。第二,使用实际飞机进行了飞行试验,以测量飞行期间飞行员的眼球运动,包括飞机经历失速时。结果表明,正确的驾驶和准确的决策是必要的,由飞行员保持正确的飞机姿态,即使在飞机经历失速。最后,研究了飞机失速时的飞行动力学特性,以预测飞机的失速特性。
项目成果
期刊论文数量(3)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
本田健一郎, 李家賢一, 砂田保人: "単独計器飛行時のワークロード評価法に関する研究"日本航空宇宙学会論文集. 48. 265-272 (2000)
Kenichiro Honda、Kenichi Rie、Yasuto Sunada:“单独仪表飞行时的工作负载评估方法的研究”日本航空学会学报48。265-272(2000)。
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- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Kenichiro Honda, Kenichi Rinoie and Yasuto Sunada: "Workload Measurements on Simulated Single Pilot Instrument Flight"Journal of Japan Society for Aeronautical and Space Science. Vol. 48, No. 559. 265-272 (2000)
Kenichiro Honda、Kenichi Rinoie 和 Yasuto Sunada:“模拟单飞行员仪表飞行的工作负载测量”日本航空航天学会杂志。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
本田健一郎,李家賢一,砂田保人: "単独計器飛行時のワークロード評価法に関する研究"日本航空宇宙学会論文集. 48巻559号. 265-272 (2000)
Kenichiro Honda、Kenichi Rie、Yasuto Sunada:“单独仪表飞行时的工作负载评估方法的研究”,日本航空学会学报,第 48 卷,第 559 期。265-272(2000 年)。
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- 影响因子:0
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RINOIE Kenichi其他文献
Verification of Optimum Spanwise Lift Distribution Design Method Applying VLM
应用VLM验证最佳展向升力分布设计方法
- DOI:
10.2322/jjsass.66.31 - 发表时间:
2018 - 期刊:
- 影响因子:0
- 作者:
ODA Yuki;YUHARA Tatsunori;RINOIE Kenichi - 通讯作者:
RINOIE Kenichi
Instantaneous Surface Pressure Measurements of Quasi-Periodic Behavior of Laminar Separation Bubble in the Angles of Attack Near Airfoil Stall
翼型失速附近攻角层流分离气泡准周期行为的瞬时表面压力测量
- DOI:
10.2322/jjsass.65.168 - 发表时间:
2017 - 期刊:
- 影响因子:0
- 作者:
FUJIWARA Go;SUNADA Yasuto;RINOIE Kenichi - 通讯作者:
RINOIE Kenichi
Plasma-assisted Hypersonic Flow Control and Aerodynamic Research at University of Tokyo
东京大学等离子体辅助高超音速流动控制和空气动力学研究
- DOI:
- 发表时间:
2017 - 期刊:
- 影响因子:0
- 作者:
ODA Yuki;YUHARA Tatsunori;RINOIE Kenichi;Yasumasa Watanabe - 通讯作者:
Yasumasa Watanabe
RINOIE Kenichi的其他文献
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{{ truncateString('RINOIE Kenichi', 18)}}的其他基金
Development of Airfoil Stall Suppression System Utilizing Smart Structure Sensor Actuators
利用智能结构传感器执行器开发机翼失速抑制系统
- 批准号:
21360412 - 财政年份:2009
- 资助金额:
$ 25.66万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Research on Airfoil Stall Suppression Control by Use of a Smart-structure Device
智能结构装置机翼失速抑制控制研究
- 批准号:
17360406 - 财政年份:2005
- 资助金额:
$ 25.66万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
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