The development undertaken was the interface circuits and equipment to permit the information in the SECANT System to be recorded in digital form for automatic processing. Two VECAS Systems were fabricated, assembled, and tested. Two sets of special test equipment consisting of a Calibration Generator and a Traffic Simulator were fabricated, assembled, and tested.
SECANT VECAS Flight Test and Evaluation Equipment
1973
126 pages
Report
Keine Angabe
Englisch
Transportation Safety , Aviation safety , Air traffic control systems , Transponders , Altitude , Coding , L band , Data transmission systems , Avionics , Digital systems , Collision avoidance , SECANT(Separation and Control of Aircraft using Nonsynchronous Techniques) , Separation and control of aircraft using nonsynchronous techniques
Flight test evaluation of Secant Vecas collision avaoidance system.(Final rept.)
Tema Archiv | 1974
|SECANT VECAS flight test and aviation equipment (final rept. 21 jul 72-31 may 73)
Tema Archiv | 1973
|Secant-method adjustment for structural models
Tema Archiv | 1991
|Secant-method adjustment for structural models
AIAA | 1989
|