The resultant of the first integration of the output from the east/west accelerometer of an inertial navigation system (INS) in NAV MODE is:4
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The resultant of the first integration from the north/south accelerometer of an inertial navigation system (INS) in the NAV MODE is:4
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What is the name given to an Inertial Reference System (IRS) which has the gyros and accelerometers as part of the unit's fixture to the aircraft structure?4
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The data that needs to be inserted into an Inertial Reference System in order to enable the system to make a successful alignment for navigation is:4
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Which of the following statement is correct concerning gyro-compassing of an inertial navigation system (INS)?4
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Which of the following statements concerning the alignment procedure for Inertial Navigation Systems(INS)/Inertial Reference Systems (IRS) at mid-latitudes is correct?4
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After alignment of the stable platform of an Inertial Navigation System, the output data from the platform is:4
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With reference to an inertial navigation system (INS), the initial great circle track between computer inserted waypoints will be displayed when the control display unit (CDU) is selected to:4
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ATT Mode of the Inertial Reference System (IRS) is a back-up mode providing:4
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Waypoints can be entered in an INS memory in different formats. In which of the following formats can waypoints be entered into all INS's?4
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Other exam subjects ATPL - Airline Transport Pilot license