The ride quality experienced by passengers is a function of airframe rigid-body, elastic dynamic responses, autopilot, and stability augmentation system control inputs. A frequency response method has been developed to select sinusoidal elevator input time histories yielding vertical load factor distributions, within a given limit, as a function of fuselage station. The numerical technique is illustrated by applying two-degree-of-freedom short-period and first symmetric mode equations of motion to a B-1 aircraft at Mach 0.85 during sea level flight conditions.
Ride quality flight testing
1978-04-01
Sonstige
Keine Angabe
Englisch
AIAA | 1978
|Ride-quality testing under controlled flight conditions
AIAA | 1975
|Ride-quality testing under controlled flight conditions
NTRS | 1975
|Flight research experiments on ride quality
NTRS | 1975
|Flight Research Experiments on Ride Quality
NTIS | 1975
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