INERTIAL NAVIGATION SYSTEM

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Q1
#1. INS errors are classified as “Bounded errors” and “Unbounded errors”.
Q2
#2. Two checks that can be carried out to check that two selected sequential waypoints have been entered correctly are:
Q3
#3. In an INS the E/W accelerations are converted into an E/W speed (kt) at the first stage of integration and into E/W distance gone (nm) at the second stage of integration. This gives:

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You’re seeing 3 sample questions. Create an account to unlock the full set and track your score.

Answered 0/3

Q1
#1. INS errors are classified as “Bounded errors” and “Unbounded errors”.
Q2
#2. Two checks that can be carried out to check that two selected sequential waypoints have been entered correctly are:
Q3
#3. In an INS the E/W accelerations are converted into an E/W speed (kt) at the first stage of integration and into E/W distance gone (nm) at the second stage of integration. This gives:

Answered 0/3

INERTIAL NAVIGATION SYSTEM — OXFORD · Docpilot