The Maneuver Criteria Evaluation Program (MCEP) is a digital computer program that solves the flight path equation of motion for a helicopter without auxiliary propulsion. The use of basic work, energy, and power relationships makes possible accurate representation of flight path trajectories. MCEP can be used to aid in the development of maneuver requirements that provide the necessary maneuver capability to perform the desired mission. The desired mission is simulated in MCEP by using individual flight controllers to 'fly' the helicopter through the mission profile. Key maneuver parameters are monitored throughout the flight profile to provide insight into the performance of the helicopter in achieving the desired flight trajectory. Three maneuvers have been modified to allow rotor rpm to be bled to use some of the rotor's stored energy. These maneuvers are a constant altitude acceleration maneuver, a collective pop-up maneuver, and a sideward acceleration maneuver. Correlation with flight test data is established to validate the bleed rpm maneuvers. The appendix to the report, the User's Guide, contains the detailed information necessary for setting up an input data deck for MCEP. (Author)
Improved Maneuver Criteria Evaluation Program
1979
82 pages
Report
Keine Angabe
Englisch
Aeronautics , Aircraft , Flight maneuvers , Helicopters , Acceleration , High energy , Helicopter rotors , Flight paths , Ground effect , Mission profiles , Terrain avoidance , Maneuverability , Computer programs , Digital simulation , Mathematical models , MCEP computer program , H-58 aircraft , OH-58A aircraft
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