Betekenis van:
navigational instrument

Voorbeeldzinnen

1. Integrated flight instrument systems, which include gyrostabilisers or automatic pilots, designed or modified for use in space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104; c. 'Integrated navigation systems', designed or modified 'missiles' and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less. Technical Notes:
2. An operator shall not operate an aeroplane in accordance with Instrument Flight Rules (IFR) or by night in accordance with Visual Flight Rules (VFR) unless it is equipped with the flight and navigational instruments and associated equipment and, where applicable, under the conditions stated in the following subparagraphs:
3. An operator shall not operate an aeroplane in accordance with instrument flight rules (IFR) or by night in accordance with visual flight rules (VFR) unless it is equipped with the flight and navigational instruments and associated equipment and, where applicable, under the conditions stated in the following subparagraphs:
4. Integrated flight instrument systems, which include gyrostabilisers or automatic pilots, designed or modified for use in space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104; c. 'Integrated navigation systems', designed or modified 'missiles' and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less. Technical Notes: 1. An 'integrated navigation system' typically incorporates the following components:
5. Integrated flight instrument systems, which include gyrostabilisers or automatic pilots, designed or modified for use in space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104; c. 'Integrated navigation systems', designed or modified for space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104 and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less. Technical Note: An 'integrated navigation system' typically incorporates the following components: 1. An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system); 2.
6. Inertial or other equipment using accelerometers specified in 7A001 or 7A101 or gyros specified in 7A002 or 7A102 and systems incorporating such equipment; Note: 7A103.a. does not specify equipment containing accelerometers specified in 7A001 where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in downhole well services operations. b. Integrated flight instrument systems, which include gyrostabilisers or automatic pilots, designed or modified for use in space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104; c. 'Integrated navigation systems', designed or modified 'missiles' and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less. Technical Notes: