The AN/ASN-163 Miniaturized Airborne Global Positioning System Receiver (MAGR) provides Over-The-Horizon navigation and secure navigation capabilities using satellite information. Back-up navigation is achieved by using heading and attitude inputs from AN/USN-2 Standard Attitude Heading Reference System (SAHRS) along with velocity and altitude inputs from the Air Data Computer.ĪN/ASN-163 Miniaturized Airborne Global Positioning System Receiver (F-14D). The AN/ASN-139 DINS includes its own computer, which performs inertial alignment and station keeping functions. The AN/ASN-139 Digital Inertial Navigation System (DINS) provides aircraft attitude, attitude rates, and velocities to the AIU. The EGI began replacing the CAINS I in August 1998.ĪN/ASN-139 Digital Inertial Navigation System (F-14D). The EGI provides three independent navigation solutions: Inertial only, GPS only, and blended GPS-INS. The Standard Central Air Data Computer (SCADC) provides air data information used for flight control, navigation, and weapon release functions.Įmbedded Global Positioning System and Inertial Navigation System (F-14B). Standard Central Air Data Computer (F-14A/B/D). Interface with equipment not compatible with the MIL-STD-1553B DMDB is provided by the AIU and CIU. The two MIL-STD-1553B DMDBs service each of the tactical computers.
F14 COCKPIT SOFTWARE
The Bulk Store Memory Unit is used to store software programs and data necessary for both ground support and in-flight operation. The second AN/AYK-14 computer acts as the radar controller and avionics Backup Bus Controller. One AN/AYK-14 acts as the avionics bus controller and radar Backup Bus Controller. The Tactical Computer System consists of two AN/AYK-14 Tactical Computers, a Bulk Store Memory Unit, AIU, CIU, and two MIL-STD-1553B DMDBs. The pilot air combat maneuvering panel, throttles, stick grip, and emergency jettison panel were modified to support the AN/AYQ-15 SMS and weapon systems. The AN/AYQ-15 Stores Management System (SMS) uses a programmable processor, decoders, and fuel tank jettison units interfaced with a MIL-STD-1553B DMDB to provide the control and logic necessary to prepare, fire, and jettison all stores.
It is integrated into the avionics system through the security and cockpit audio equipment.ĪN/AYQ-15 Stores Management System (F-14D). The AN/ARC-182 Very High Frequency (VHF)/Ultra High Frequency (UHF) provides two way simplex plain and cryptographic voice communication. The Computer Interface Unit (CIU) converter provides signal conditioning and data formatting necessary to interface the MIL-STD-1553B DMDB with radar equipment that is not data bus compatible.ĪN/ARC-182(V) Very High Frequency/Ultra High Frequency - Amplitude Modulated/Frequency Modulated HAVE QUICK (F-14A/B/D). The Avionics Interface Unit (AIU) converter provides signal conditioning and data formatting necessary to interface the MIL-STD-1553B DMDB with avionics equipment that is not data bus compatible.Ĭomputer Interface Unit (F-14D). The MX-10666/A Adaptive Interference Blanker provides signal blanking compatibility.Īvionics Interface Unit (F-14D). The MIL-STD-1553D DMDB allows for new avionics subsystems to be integrated and employed by changing bus control software. MIL-STD-1553B Digital Multiplex Data Bus (F-14B/D). The new high technology engine improves capability and maneuverability without throttle restrictions or engine trimming. The F110-GE-400 is a new design that emphasizes reliability, maintainability, and operability. The F-14B and F-14D Aircraft are equipped with two F110-GE-400 engines. The F-14A is equipped with two TF30-P-414A Turbofan Jet Engines.
0 kommentar(er)
