22-06. AEROPLANE: AUTOMATIC FLIGHT CONTROL SYSTEMS
Всего заданий: 100
В режиме ОБУЧЕНИЕ показываются все задания дисциплины с предъявлением правильных ответов. Для перехода к следующему заданию нажать кнопку «Далее».
Заданий на экзамен: 10
В режиме ЭКЗАМЕН правильные ответы не показываются, переход на следующее задание происходит автоматически, после выбора ответа.
1. The correction of the control surface deflection made by the autopilot calculator in order to keep a given altitude will be all the more significant when the:
1) difference between the attitude necessary to keep the given or reference altitude and the instantaneous attitude is high.
2) variation speed of the difference between the attitude necessary to maintain the altitude and the instantaneous attitude is high.
3) difference between the altitude of reference and the instantaneous altitude is high.
4) variation speed of the difference between the reference altitude and the instantaneous altitude is high.
The combination re-grouping the correct statements is:
2. The purpose(s) of the flight director system is (are) to:
1) give the position of the aircraft according to radioelec- tric axis
2) give the position of the aircraft according to waypoints
3) to aid the pilot when flying manually
The combination regrouping all the correct statements is:
3. The «heading hold» mode is selected on the flight director (F
4. (Refer to figure 022-01)
After having programmed your flight director, you see that the indications of your ADI (Attitude Director Indicator) are as represented in the diagram of the figure. On this instrument, the command bars indicate that you must bank your airplane to the left and:
5. If only a single A/P is used to climb, cruise and approach; following a failure of an inner loop component:
