The objective of the present dissertation is to show how redundant control surfaces can be exploited to shape an aircraft dynamic behavior and obtain desired flight mechanics performance.
This is achieved by introducing novel approaches and methods for flight mechanics and control, mainly revolving around original implementations of traditional formulations of the Control Allocation (CA) problem. The CDU/MCDU is available on screen or in 3D hardware. Training is presented on a large curved display screen with a high performance workstation. Offroad Jeep Driving Jeep Game APK Download for Android. Control surfaces and, more in general, control effectors are defined as redundant if they are capable to independently control the same motion axis of the aircraft. Desktop Trainers The MPS desktop trainers are great tools to help students to get acquainted with the FMS and are available for the B737 and A320. In the meantime, please feel free to search for ways to make a difference in your community at. Redundant effectors can be linked together, and to the pilot input, in many ways according to different optimality criteria and/or performance objectives. The latter is intended as the ability to use control effectors to alter the aircraft lift "without, or largely without, significant change in the aircraft incidence, and ideally is meant not to generate pitching moment." In particular, the research presented in this dissertation focuses on the possibility to achieve Direct Lift Control (DLC). The ability to do so is essentially dependent on the position of the Control Center of Pressure (CCoP), which is the center of pressure of aerodynamic forces solely due to control surface deflections.
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