‘Integrated navigation systems’, designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of 200 m CEP or less.

Items, materials, equipment, goods and technology related to ballistic missile programmes

CATEGORY II ITEM 9 - INSTRUMENTATION, NAVIGATION AND DIRECTION FINDING

S/2012/947

Technical Note: An ‘integrated navigation system’ typically incorporates all of the following components: a. An inertial measurement device (e.g. an attitude and heading reference system, inertial reference unit, or inertial navigation system); b. One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g. satellite navigation receiver, radar altimeter, and/or Doppler radar); and c. Integration hardware and software. N.B. For integration “software”, see Item 9.D.4.