Guided Missile Altitude Control
Item Name Code (INC) 00911
![]() |
A specifically designed control which is manually preset to establish maximum altitude of a guided missile's flight. May include facilities for presetting final dive angle. Excludes CONTROL, ALTITUDE, AUTOMATIC PILOT and CONTROLLER, FLIGHT, AUTOMATIC PILOT.
Additional Information for Guided Missile Altitude Control
Guided Missile Altitude Control refers to the components or systems that are responsible for controlling and maintaining the altitude of a guided missile during its flight. These components are part of the supply class Guided Missile Components, which falls under the supply group Guided Missiles.
The altitude control system of a guided missile is crucial for its successful navigation and targeting. It allows the missile to maintain a specific altitude, whether it is flying at low altitudes to avoid detection or at higher altitudes to cover longer distances.
The altitude control system typically consists of various components, such as altitude sensors, actuators, and control algorithms. The altitude sensors measure the current altitude of the missile, while the actuators adjust the missile's control surfaces or propulsion system to maintain the desired altitude.
The control algorithms process the altitude sensor data and provide commands to the actuators, ensuring that the missile stays on the desired altitude trajectory. These algorithms may take into account factors such as wind conditions, target altitude requirements, and mission objectives.
Overall, Guided Missile Altitude Control is a critical aspect of guided missile technology, enabling precise and effective targeting capabilities.
Related Item Names for INC 00911 Guided Missile Altitude Control
NATO Stock Numbers with Item Name 00911 Guided Missile Altitude Control Page 1 of 1
- 9599 607 11301
- RNCC: 5 | RNVC: 2 | DAC: 4
- 537081
- RNCC: 6 | RNVC: 9 | DAC: 9
- VG95211-ML-127029046
- RNCC: 2 | RNVC: 2 | DAC: 3