EFFECTS OF ENGINE AND HEIGHT-CONTROL CHARACTERISTICS ON HELICOPTER HANDLING QUALITIES.

被引：0

作者：

Corliss, Lloyd D.

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来源：

Journal of the American Helicopter Society | 1983年 / 28卷 / 03期

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D O I：

10.4050/jahs.28.3.56

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摘要：

A ground-based simulation study was conducted on a large-scale motion simulator to study the effects in the vertical axis of engine response characteristics on handling qualities for a nap-of-the-earth (NOE) operating environment. This study concentrated specifically on the helicopter configuration with a speed-governed gas-turbine engine and expands previous work by focusing on aspects peculiar to rotary-wing and NOE operations. A wide range of engine response time, vehicle damping and sensitivity and excess power levels was studied.

引用

页码：56 / 62

共 28 条

[1] INFLUENCE OF ENGINE/FUEL CONTROL DESIGN ON HELICOPTER DYNAMICS AND HANDLING QUALITIES.
Kuczynski, W.A.
Copper, D.E.
Twomey, W.J.
Howlett, J.J.
Journal of the American Helicopter Society, 1980, 25 (02) : 26 - 34
[2] INFLUENCE OF ENGINE/FUEL CONTROL DESIGN ON HELICOPTER DYNAMICS AND HANDLING QUALITIES.
Kuczynski, W.A.
Cooper, D.E.
Twomey, W.J.
Howlett, J.J.
Applications of Cryogenic Technology, 1979,
[3] EVALUATIONS OF HELICOPTER INSTRUMENT - FLIGHT HANDLING QUALITIES.
Sinclair, S.R.M.
Kereliuk, S.
Aeronautical Report (National Research Council Canada), 1982,
[4] REVIEW OF THE EFFECTS OF SIDE-STICK CONTROLLERS ON ROTORCRAFT HANDLING QUALITIES.
Aiken, Edwin W.
Journal of the American Helicopter Society, 1986, 31 (03) : 27 - 34
[5] Helicopter Handling Qualities: A study in pilot control compensation
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Journal of the American Helicopter Society, 1982, 27 (01) : 35 - 41
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[8] Vision-based control for helicopter ship landing with handling qualities constraints
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IFAC PAPERSONLINE, 2016, 49 (17): : 118 - 123
[9] Robust Multivariable Sliding Mode Attitude Control for Enhanced Helicopter Handling Qualities
Halbe, Omkar
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[10] DESIGN OF A MULTIVARIABLE HELICOPTER FLIGHT CONTROL-SYSTEM FOR HANDLING QUALITIES ENHANCEMENT
GARRARD, WL
LIEBST, BS
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1990, 35 (04) : 23 - 30

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