Aeronautics and Human-Engineering Joint Research to Avoid Aircraft Stall Accidents
Aeronautics and Human-Engineering Joint Research to Avoid Aircraft Stall Accidents
批准号:
10305072
负责人:
RINOIE Kenichi
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
项目状态:
已结题
起止时间:
1998 至 2001
中文摘要
当飞机机翼迎角增大时,在一定迎角处升力会突然减小。这称为机翼失速,也是飞机事故的原因之一。为了避免飞机失速事故,不仅需要考虑飞机的飞行动力学方面,还需要考虑飞行员的人体工程学方面。本研究的目的是从飞行动力学和人体工程学两个角度阐明飞行员的失速避免和改出技术。本研究对空气动力学和飞行动态失速特性、驾驶技术和飞行员工作负荷进行了研究。首先,使用飞行模拟器进行了飞行员工作负荷测量,以调查飞行员技能和飞行员工作负荷。建立了以飞行员信息处理为主的飞行员工作负荷评价方法。结果表明,经验不足的飞行员在整个飞行过程中的工作量一直很高。高工作量妨碍了准确和正确的决策,从而进一步增加了工作量。其次,使用实际飞机进行了飞行测试,以测量飞行过程中飞行员的眼球运动,包括飞机失速时的眼球运动。结果表明,即使飞机失速,飞行员的正确驾驶和准确决策对于保持飞机正确的姿态也是必要的。还讨论了眼睛扫描到适当仪器的重要性。最后,研究了飞机经历失速时的飞行动力学特性,以预测飞机失速特性。
英文摘要
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.
期刊论文(3)
专著(0)
科研奖励(0)
会议论文
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)。
DOI:
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发表时间:
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影响因子:
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作者:
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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:
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发表时间:
期刊:
影响因子:
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作者:
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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)。
DOI:
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发表时间:
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影响因子:
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作者:
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通讯作者:
Development of Airfoil Stall Suppression System Utilizing Smart Structure Sensor Actuators
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批准号:21360412
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$10.82万
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财政年份:2009
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负责人:RINOIE Kenichi
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依托单位:
Research on Airfoil Stall Suppression Control by Use of a Smart-structure Device
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批准号:17360406
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$7.62万
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财政年份:2005
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负责人:RINOIE Kenichi
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依托单位:
海外基金