Neural Network Based Helicopter Low Airspeed Indicator
Abstract
This invention relates generally to virtual sensors and, more particularly, to a means and method utilizing a neural network for estimating helicopter airspeed at speeds below about 50 knots using only fixed system parameters (i.e., parameters measured or determined in a reference frame fixed relative to the helicopter fuselage) as inputs to the neural network.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 24, 1996
- Accession Number
- ADD018857
Entities
People
- Carl Schaefer Jr.
- David Haas
- Kelly Mccool
Organizations
- United States Department of the Navy