![]() ![]() The entire system is interfaced with computer so that the entire control unit is managed by a special VB program written on. This additional voltage is obtained from the comparator and feedback to the stepper motor. The required actuation is not obtained due to the aerodynamic disturbances, and so, the actual actuation in the control surfaces introduces overloading in the stepper motor resulting in the requirement of additional voltage for actuation. The main control console unit includes microcontroller, stepper motor, DC gear motor, relays and voltage regulators light source, and receiver. In the analysis, digital control system is used and merged with the light intensity in the control surface actuation. NASA Research Test Pilot Neil Alden Armstrong conducts a flight to test the Minneapolis-Honeywell MH-96 flight control system installed in the third North. This paper overviews the development of the digital fly-by-wire Flight Control System FCS in the FA-18 aircraft. ![]() Aircraft axes of control An aircraft has three main axes. When the moving part or the surface is moved, the aerodynamic characteristic of the main surface is changed which allows the aircraft to be maneuvered by the pilot. Thales Flight Control Systems on board major programs. In almost all aircraft, the flight controls are movable aerodynamic surfaces attached to a main lifting body. So, it is required to develop an aircraft which gives the expected actuation by overcoming aerodynamic loading and presence of any other obstacles. Thales has grown to become the largest flight control electronics system supplier in the world. These actuators may fail to give the expected actuation due to aerodynamic loading and presence of any other obstacles. In a commercial aircraft, the control surfaces are controlled and actuated using hydraulic or pneumatic or servo actuators. ![]()
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