22-05. INERTIAL NAVIGATION AND REFRENCE SYSTEMS (INS and IRS)
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1. In an Inertial Reference System, accelerations are measured in relation to:
2. The resultant of the first integration of the output from the east/west accelerometer of an inertial navigation system (INS) in NAV mode is:
3. On the IRS, selection of ATT mode gives:
4. Double integration of the output from the east/west accelerometer of an inertial navigation system (INS) in the NAV mode gives:
5. A laser reference system (IRS), as compared to a gyro reference system (INS):