22-05. INERTIAL NAVIGATION AND REFRENCE SYSTEMS (INS and IRS)
All questions: 87
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1. The azimuth gyro of an Inertial Navigation Unit has a drift of 0,01°/h. After a 12-hour flight with a ground speed of 500 kts, the error on the aeroplane position is approximately:
2. The principle of a laser gyro is based on:
3. What method of entering waypoints can be used on all INS equipment?
4. During initial alignment an inertial navigation system is north aligned by inputs from:
5. Which of the following statement is correct concerning gyro-compassing of an inertial navigation system (INS)?
