The integration of the Total Energy Control System (TECS) concept with 4D navigation is described. This integration was made to increase the operational capacity of modern aircraft and encourage incorporation of this increased capability with the evolving National Airspace System (NAS). Described herein is: 4D smoothing, the basic concepts of TECS, the spoiler integration concept, an algorithm for nulling out time error, speed and altitude profile modes, manual spoiler implementation, 4D logic, and the results of linear and nonlinear analysis.
4D-TECS (Total Energy Control System) Integration for NASA (National Aeronautics and Space Administration) TSRY Airplane
1989
168 pages
Report
Keine Angabe
Englisch
4D-TECS integration for NASA TCV airplane
AIAA | 1988
|National Aeronautics and Space Administration (NASA)
TIBKAT | 2020
|