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Stability and Control Harmony in Approach and LandingA review of the factors which affect stability and control harmony in approach and landing is made to obtain a clearer understanding of the proper relationship, the trade-offs involved, and to show how limits in stability and control harmony are established for advanced aircraft. Factors which influence stability and control harmony include the longitudinal short period response of the aircraft and the level of several pitch control characteristics including control power, control sensitivity, and control feel. At low stability levels for advanced aircraft, less conventional control techniques such as DLC are needed to improve harmony and some form of stability augmentation must be provided to improve precession of flight path control and reduce pilot work load.
Document ID
19750013155
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, S. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: AGARD Take-off and Landing
Subject Category
Aircraft Stability And Control
Accession Number
75N21227
Distribution Limits
Public
Copyright
Other
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