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A low-cost inertial smoothing system for landing approach guidanceAccurate position and velocity information with low noise content for instrument approaches and landings is required for both control and display applications. In a current VTOL automatic instrument approach and landing research program, radar-derived landing guidance position reference signals, which are noisy, have been mixed with acceleration information derived from low-cost onboard sensors to provide high-quality position and velocity information. An in-flight comparison of signal quality and accuracy has shown good agreement between the low-cost inertial smoothing system and an aided inertial navigation system. Furthermore, the low-cost inertial smoothing system has been proven to be satisfactory in control and display system applications for both automatic and pilot-in-the-loop instrument approaches and landings.
Document ID
19730015926
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Niessen, F. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Navigation
Report/Patent Number
L-8763
NASA-TN-D-7271
Report Number: L-8763
Report Number: NASA-TN-D-7271
Accession Number
73N24653
Funding Number(s)
PROJECT: RTOP 760-63-04-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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