1. Mini Autonomous Flying Vehicle CASDE is part of the National effort to develop a Micro Air Vehicle. CASDE has chosen a Mini Vehicle, in the short term, keeping in mind the autonomous mission. CASDE feels that ~500 Gms. of Avionics is bare minimum to make a mission autonomous. A 2 Kg. Aircraft, with 500-600 Gms. payload, needs to be demonstrated.

2. Mini Flying Vehicle Scenario

3. CASDE’s Approach Instrumented Flying Platform Aircraft Fabrication and Instrumentation Correlation of Mission with Flight data Videography Platform, Solar Powered Aircraft SE Approach to Design & Development Mission Realization Avionics Development & Integration Studies Autonomous Mission Implementation

4. Instrumented Flying Platform Span - 1.7 mChord - 29.5 cm Fuselage length - 1.07 m Weight - 3800 gm (fuel)Weight of Inst. - 500 gm Engine Disp. - 7.5 ccPower - 1.6 BHP Parameters: N x N y N z q h v  e 

5. Instrumented Flying Platform Recorded Flight Data for a Loop

6. Design & Build an Aerial Vehicle Capable of Carrying a Video Camera/ Transmitter. A circle & Two Rectangles as Targets for Videography Maximum Dimension 24” & All- Up-Weight Less Than 1 kg. Distance 500m Target Launch Videography Platform Wing Airfoil- Selig 3021 - 095 -84 Wing Span- 24” (both wings) Wing Chord- 6” Wing Gap- 4.25” Wing Area- 288 sq. in (2 sq. ft) Fuselage - 23.5” Tail span- 14” Tail Chord- 4.5” Tail Arm- 12.25” Max AUW- 860 gm (30.27 oz) Wing loading- 15.14 oz/sq. ft

7. Videography Platform

8. Solar Powered Aircraft Span : 90 cm Aspect ratio : 8 Power requirement : 4 watts Solar Panel weight : 70 grams Total weight : 140 grams

9. Avionics Development & Integration Components off the Shelf Selection and Integration Weight, Size & Performance as Criterion

10. CASDE MAV Configuration Fixed Wing with Speed of 10-35 Metres/Sec. Avionics Payload of ~ 500-700 Grams Autonomous Flight Capability Way Point (with Mission) Based Navigation Range of ~ 5 km & Endurance of 30 Minutes Video Surveillance & Live Transmission Stabilized Platform for Good Picture Quality

11. Aircraft SARIKA-II of IIScOR Instrumented Flying Aircraft of CASDE Navigation, Guidance and Control Strategy NGC Developed by ADE for Nishant to be used Avionics Package to be Developed by CASDE Simulations Ground Based Off-line, OILS, AILS & Mission CASDE MAV Development Strategy

12. Avionics & Videography Packages Sensor/PayloadWeight (grams) Controller / Data Logger65 3-axis Accelerometer30 2-axis Rate Sensor25 Pressure Based Altimeter15 Pressure Based Airspeed15 Heading Sensor10 GPS Receiver100 GPS Antenna50 Angle Of Attack Sensor15 9V Batteries for One Hour100 Total Components’ Weight425 15-20 % for filters, wiring75 Total weight500 EquipmentWeight (grams) TV Quality Camera 20 5 km range Transmitter 20 * 1 Hour duration Battery 50 Total weight90 * It is an estimate, as transmitter for 300 m weighs 10 Gms. Autonomous Flight Payload EstimateVideo. Mission Payload Estimate

13. FLIGHT DYNAMICS SIMULATOR GPS SIMULATOR SENSOR MODEL D/A RS232 A/D NAVIGATION GUIDANCE AND CONTROL SYSTEM A/DRS232 ACTUATING COMMANDS ACTUATORS AND POTENTIOMETERS DESKTOP COMPUTER ONBOARD SYSTEM HARDWARE IN LOOP SCHEMATIC OF HILS FACILITY