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3D Training System for Naval Aircraft Maintenance Personnel

Digital Radiance designed and developed the interactive 3D graphics for the 6E34 Gyroscope Gimbal Trainer used by the Naval Air Tactical Training Command (NATTC) at the Naval Air Station in Pensacola, Florida. The trainer concept, also designed by Digital Radiance, uses a large-screen projection system to teach the basic components and functions of the gyroscope-based inertial navigation system common to all modern aircraft. This trainer replaced a tedious mechanical mockup and has set the new standard to which all training systems are developed for NATTC.

The trainer's first section demonstrates the effects of pitch, roll, and yaw on the aircraft's gyroscope gimbal system, shown in the center of the trainer's display. To provide further context, an FA-18 jet and the pilot's Attitude-Direction Indicator (ADI) are shown in opposite corners of the trainer's display. The student can interactively manipulate the system's pitch, roll, or yaw to any angle, as seen in the following three screen snapshots, and can observe the simultaneous effects on all of the displayed elements.

Zero pitch, roll, & yaw

30 degrees yaw

30 degrees pitch, roll, & yaw

 

The trainer's second section lists the basic mechanical and electrical parts in the gyroscope gimbal system. The part names are listed at the left of the trainer's display. Each part name can be selected to highlight the corresponding part in the picture of the gyroscope gimbal system at the right of the trainer's display. A sample screen snapshot is shown below.

The gyroscope gimbal system with the "Outer Roll Gimbal" part name and the corresponding outer roll gimbal part highlighted in yellow

 

The trainer's final section demonstrates the functionality of each part in the gyroscope gimbal system as the system responds to a power-up sequence or to a 30 degree change in pitch. The following four pictures show the screen snapshots as the user changes the pitch.

1. As the system pitches down, the forward gyroscope remains fixed relative to its spin axis. It sends a difference signal, denoted by a yellow animated arrow, to the rear gyro's pitch servo.

2. The rear gyro's pitch servo then sends a corresponding signal (barely visible at this reduced size) to the rear gyro's pitch follow-up motor/generator.

3. The pitch follow-up gimbal, now highlighted in yellow, begins moving to stay synchronized with the forward gyroscope's spin axis.

4. The two gyroscope gimbals are now synchronized in pitch, allowing the rear gyro to correctly report any changes in its orientation relative to the front gyro's pitch.

 

 
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