The principle of piloted vehicle mechanics is presented, and aircraft longitudinal movement is studied. Assuming that the pilot counters with his lateral controls any sideslip, and that the aircraft plane of symmetry is vertical, the trajectory is described in that same vertical plane. The natural modes (angle of attack oscillation, phugoid, aperiodic motion) of the small movements around straight and level flight, the response to the pilots commands, and equilibrium stability, are examined. Small lateral movements around straight and level flight and the aircraft response to lateral controls are considered. Small movements of the aircraft around stabilized level flight in rotation are also examined. The assumptions of separation of longitudinal and lateral movements around stabilized straight and level flight are validated.
Flight Dynamics and Aircraft Piloting
1985
419 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamic stability , Aeronautical engineering , Aircraft control , Flight characteristics , Flight mechanics , Pilot performance , Attitude stability , Directional stability , Horizontal flight , Human reactions , Lateral stability , Longitudinal control , Foreign technology , Translations
Flight Dynamics and Aircraft Piloting
NTIS | 1983
|Flight Dynamics and Aircraft Piloting
NTIS | 1976
|Engineering Index Backfile | 1959
|Engineering Index Backfile | 1936
|METHOD OF CONTROLLING OPERATION OF AIRCRAFT PILOTING DEVICE AND AIRCRAFT PILOTING DEVICE
Europäisches Patentamt | 2018
|