The instruments and data evaluation used for flight testing of two Litton laser gyro strapdown navigation systems in a DO-28 aircraft are described. The reference data based on the platform navigation system CAROUSEL 4a are corrected by application of optimal smoothing techniques. Results of the LTN-90 flight tests are presented and graphs of one of the flight tests are discussed.
Flight Testing of Litton Laser Gyro Strapdown System LTN-90 for General Aviation
1984
43 pages
Report
No indication
English