1. Chassis Interfaces Interface to Plane Small Passenger AircraftRIT U.A.V. Airframe “C” Mountable to a flat plateMountable to a flat wooden base Smaller than a person; Approx 2’ x 2’ x 5’6” tall Less than 16” x 6.5” x 5” tall Less than 150lbs (68kg)Less than 15lbs (6.8kg)

2. Chassis Interfaces Interface to Plane 10.25” Long 6” Wide 6.5” Tall 10.9lbs

3. Chassis Interfaces Interface to Plane ComponentWeight (lbs) Electronics0.91 Electronics Enclosure3.43 Optics2.15 Optics Enclosure4.32 Total11 lbs (Approximate)

4. Chassis Interfaces D3 OEM BoardNovAtel OEMV-3FPGA BoardConnector BoardSolid State Hard Drive (Not Pictured)

5. Chassis Interfaces

6. Camera BoardsLinos Mevis-C Lenses (16 mm) MicroStrain IMU

7. Chassis Interfaces

8. Vibration Damping Two sources of need: 1.Insure structural integrity under vibration 2.Minimize image distortion Item 1 must be tested for, but item 2 can be calculated and designed for.

9. Vibration Damping Characterized per RTCA DO-160 Frequency Range: 5 – 500 Hz Amplitude Range: 0.00001 – 0.1 inches 3 Primary Axes

10. Vibration Damping Image distortion depends on: – Aircraft Speed – Aircraft Altitude – Lens Image Angle – Shutter Speed

11. Vibration Damping Speed induced by vibration taken as derivative of vibration motion profile Profile: X = A·sin(F·t) Speed: X’ = A·F·cos(F·t)

12. Vibration Damping Maximum Aircraft Speed: 36 m/s Maximum Vibration Speed: 1.27 m/s Altitude (ft) Speed Distortion (Pixels) Vibration Distortion (Pixels) 1000 0.660.0233 1500 0.440.0155 2000 0.330.0116 5000 0.130.0047