Q. The velocity at which yawing motion can be produced by rudder deflection while the aircraft is on the ground is called _______

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Q. Departure and approach are subphases of what?

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Q. The height at which approach is aborted when the runway is not in sight is called as?

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Q. A non-precision approach has electronic guidance in only in the horizontal direction.

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Q. What instrument is used to measure the aircraft’s altitude during the approach phase?

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Q. Which of the following conditions does not lead to missed approaches?

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Q. The navigation equations are used by the on-board computer to calculate position velocity and altitude.

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Q. Which one of the following is not an input utilized by the aircraft navigation system?

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Q. What is the angle between the normal to the reference ellipsoid and the equatorial plane at a point called?

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Q. Which of the following is false with respect to Earth centered inertial coordinate system?

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Q. Which coordinate system is used in satellite based radio navigation?

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Q. Geocentric spherical coordinates are used for short range dead reckoning navigation.

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Q. What is the technique of calculating position from measurements of velocity called?

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Q. The angle of arrival, relative to the airframe, of a radio signal from an external transmitter is called _________

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Q. ________ related ranging errors to the dispersion in measured position?

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Q. What is TDOP?

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Q. Received radio energy is a function of the area of the receiving antenna.

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Q. The ratio of terminating impedance to the power density of the incident wave is called as?

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Q. The factor by which a receiver fails to reach the theoretical internal noise limit is known as ________

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Q. What is the maximum limit on the frequency that can be used for ground wave communication?

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