A seventy hour flight test program was performed to determine the suitability and accuracy of a low cost Omega navigation receiver in a general aviation aircraft. An analysis was made of signal availability in two widely separated geographic areas. Comparison is made of the results of these flights with other navigation systems. Conclusions drawn from the test experience indicate that developmental system improvement is necessary before a competent fail safe or fail soft area navigation system is offered to general aviation. (Author)
Flight Test and Evaluation of omega Navigation for General Aviation
1975
266 pages
Report
Keine Angabe
Englisch
Flight test and evaluation of Omega navigation for general aviation
DSpace@MIT | 1975
|Omega navigation for general aviation
AIAA | 1976
|