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Development of a takeoff performance monitoring systemThe development and testing of a real-time takeoff performance monitoring system is discussed. The algorithm is madeup of two segments: a pretakeoff segment and a real-time segment. One-time inputs of ambient conditions and airplane configuration information are used in the pretakeoff segment to generate schedule performance data for that takeoff. The real-time segment uses the scheduled performance data generated in the pretakeoff segment, runway length data, and measured parameters to monitor the performance of the airplane throughout the takeoff roll. Airplane and engine performance deficiencies are detected and annunciated. An important feature of this algorithm is the one-time estimation of the runway rolling friction coefficient. The algorithm was tested using a six degree of freedom airplane model in a computer simulation. Results from a series of sensitivity analysis are also included.
Document ID
19860022119
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srivatsan, R.
(Kansas Univ. Lawrence, United States)
Downing, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Bryant, W. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:89001
NASA-TM-89001
Report Number: NAS 1.15:89001
Report Number: NASA-TM-89001
Meeting Information
Meeting: AIAA Guidance
Location: Navigation and Control Conference, Williamsburg, VA
Country: United States
Start Date: August 18, 1986
End Date: August 20, 1986
Accession Number
86N31591
Funding Number(s)
PROJECT: RTOP 505-66-41-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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