Betekenis van:
inertial navigation

inertial navigation
Zelfstandig naamwoord
    • a method of controlling the flight of a missile by devices that respond to inertial forces

    Synoniemen

    Hyperoniemen


    Voorbeeldzinnen

    1. Inertial navigation systems
    2. An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system);
    3. Note:Flight control and navigation systems in 7A103.d. include gyrostabilizers, automatic pilots and inertial navigation systems.
    4. An autonomous flight control and navigation capability (e.g., an autopilot with an Inertial Navigation System); or
    5. Inertial navigation systems or gyro-astro compasses, containing accelerometers or gyros, specified in 7A001 or 7A002;
    6. Inertial navigation systems or gyro-astro compasses containing accelerometers or gyros specified in 7A001 or 7A002;
    7. "Source code" for the "use" of any inertial navigation equipment, including inertial equipment not controlled by 7A003 or 7A004, or Attitude and Heading Reference Systems (AHRS).
    8. "Source code" for the "use" of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (’AHRS’).
    9. "Source code" for the "use" of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (AHRS).
    10. Inertial Navigation Systems (INS) (gimballed or strapdown) and inertial equipment designed for "aircraft", land vehicle, vessels (surface or underwater) or "spacecraft" for navigation, attitude, guidance or control and having any of the following and specially designed components therefor:
    11. Inertial Navigation Systems (INS) (gimballed or strapdown) and inertial equipment, designed for "aircraft", land vehicle, vessels (surface or underwater) or "spacecraft" for navigation, attitude, guidance or control and having any of the following and specially designed components therefor:
    12. Designed for use in inertial navigation or guidance systems and specified to function at linear acceleration levels exceeding 100 g;
    13. Designed for use in inertial navigation systems or in guidance systems of all types and usable in ’missiles’;
    14. designed for use in inertial navigation systems or in guidance systems of all types and usable in "missiles";
    15. Unmanned aerial vehicles having any of the following: a. An autonomous flight control and navigation capability (e.g., an autopilot with an Inertial Navigation System); or