Effect of an autopilot sensitive to yawing velocty on the lateral stability of a typical high-speed airplane / Ordway B. Gates, Jr., and Leonard Sternfield.
Calculations have been made to determine the effect of an autopilot sensitive to yawing velocity on the lateral stability of a fighter airplane designed for transonic or supersonic speeds. The effects of inclination of the gyro reference axis and of time lag in the autopilot are discussed. Airplane...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2470. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2470
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| Y 3.N 21/5:6/2470 | Available Place a Hold |