The primary purpose of this study was to program and simulate advanced flight command computations for flight command functions common to many missions. A systems approach is taken in making use of available aircraft sensors and/or radio information to accomplish mission objectives. The functions simulated were horizontal (area) navigation, horizontal steering, vertical navigation, pitch control, energy maneuverability (optimum climb), and automatic throttle. Both completely automatic flight and manual (display) steering were simulated. The simulation was conducted at the hybrid computation facilities of the Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio. The aircraft characteristics used were those of the F-4C. (Author)
Simulation Evaluation of Flight Command Functions
1970
237 pages
Report
Keine Angabe
Englisch
Common Carrier & Satellite , Aircraft , Jet aircraft , Command and control systems , Mathematical models , Flight control systems , Jet fighters , Display systems , Horizontal indicators , Vertical indicators , Navigation computers , Ground position indicators , Flight paths , Simulation , Computer programs , Flight command functions , Computerized simulation , F-4 aircraft , F-4c aircraft
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