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naca-report-1304

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  • November 2, 2016 Create Date
  • November 2, 2016 Last Updated
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National Advisory Committee for Aeronautics, Report - Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes

naca-report-1304-flight-investigation-of-the-effectiveness-of-an-automatic-aileron-trim-control-device-for-personal-airplanes-1

A flight investigation to determine the efiectioeness of an auto-
matic. aileron trim control device installed in a personal airplane
to augment the apparent spiral stability has been conducted.
The device utilizes a rate—gyro sensing element in order to switch
an on-ofi type of control that operates the ailerons at a fixed rate
through control centering springs. An analytical study using
phase-plane and analog-computer methods has been carried out
to deter-mine a desirable method of operation for the automatic
trim control.

Results indicate that the device is capable of maintaining the
airplane in equilibrium over its operational speed range under
directional outpof—trim conditions that would cause rapid diver-
gence of the basic airplane. The device also prevents excessive
heading wander and airplane gyrations in turbulent air without
pilot control. A means for holding the airplane in a stabilized
turn to facilitate mild maneuvering through the automatic control
is pro-aided.

As a result of the present interest in the spiral—stability
problem associated with most personal-owner airplanes, the
National Advisory Committee for Aeronautics has under—
taken a program to investigate the effectiveness of a spiral-
stability augmenting device. The specific problem facing
the pilot of a- personal—owner airplane is to maintain his air—
plane in wings-level flight during times when he has no natu-
ral-horizon reference and to keep the airplane from diverging
spirally while he may be preoccupied with navigational prob-
lems.

It is demonstrated in reference 1 that the pilot’s sense
of orientation is unreliable in the absence of a visual refer-
ence, as may be the case when inadvertently or unavoidably
encountering instrument weather. Also, many personal air-
planes are equipped with only the basic instruments for in-
strument flight (turn indicator, ball—bank indicator, alt-i-
meter, and airspeed meter). Considerable proficiency in
instrument flying is required to interpret the indications of
these instruments properly and, in many cases, personal-
airplane pilots are not sufficiently skilled in instrument flying
to undertake it with safety.

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naca-report-1304

  • Version
  • 150 Downloads
  • 1.57 MB File Size
  • 1 File Count
  • November 2, 2016 Create Date
  • November 2, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes

naca-report-1304-flight-investigation-of-the-effectiveness-of-an-automatic-aileron-trim-control-device-for-personal-airplanes-1

A flight investigation to determine the efiectioeness of an auto-
matic. aileron trim control device installed in a personal airplane
to augment the apparent spiral stability has been conducted.
The device utilizes a rate—gyro sensing element in order to switch
an on-ofi type of control that operates the ailerons at a fixed rate
through control centering springs. An analytical study using
phase-plane and analog-computer methods has been carried out
to deter-mine a desirable method of operation for the automatic
trim control.

Results indicate that the device is capable of maintaining the
airplane in equilibrium over its operational speed range under
directional outpof—trim conditions that would cause rapid diver-
gence of the basic airplane. The device also prevents excessive
heading wander and airplane gyrations in turbulent air without
pilot control. A means for holding the airplane in a stabilized
turn to facilitate mild maneuvering through the automatic control
is pro-aided.

As a result of the present interest in the spiral—stability
problem associated with most personal-owner airplanes, the
National Advisory Committee for Aeronautics has under—
taken a program to investigate the effectiveness of a spiral-
stability augmenting device. The specific problem facing
the pilot of a- personal—owner airplane is to maintain his air—
plane in wings-level flight during times when he has no natu-
ral-horizon reference and to keep the airplane from diverging
spirally while he may be preoccupied with navigational prob-
lems.

It is demonstrated in reference 1 that the pilot’s sense
of orientation is unreliable in the absence of a visual refer-
ence, as may be the case when inadvertently or unavoidably
encountering instrument weather. Also, many personal air-
planes are equipped with only the basic instruments for in-
strument flight (turn indicator, ball—bank indicator, alt-i-
meter, and airspeed meter). Considerable proficiency in
instrument flying is required to interpret the indications of
these instruments properly and, in many cases, personal-
airplane pilots are not sufficiently skilled in instrument flying
to undertake it with safety.

FileAction
naca-report-1304 Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes.pdfDownload 
17,005 Documents in our Technical Library
2727423 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...