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Integrated flight controller for light aircraftController-throttle engages spoiler/dive brake system when throttle setting is below a fixed power setting and gradually increases effect of spoiler/dive brake as throttle is moved toward idle position; since action is automatically reversible, a sudden application of power abruptly terminates aerodynamic effects of spoiler/dive brake system.
Document ID
19720000213
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Olcott, J. W. (Aeron. Res. Associates of Princeton, Inc.)
Ellis, D. R. (Aeron. Res. Associates of Princeton, Inc.)
Seckel, E. (Aeron. Res. Associates of Princeton, Inc.)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Mechanics
Report/Patent Number
ARC-10456
Report Number: ARC-10456
Accession Number
72B10213
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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