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,

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Presentation transcript:

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 Gms. payload, needs to be demonstrated.

Mini Flying Vehicle Scenario

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

Instrumented Flying Platform Span mChord cm Fuselage length m Weight gm (fuel)Weight of Inst gm Engine Disp ccPower BHP Parameters: N x N y N z q h v  e 

Instrumented Flying Platform Recorded Flight Data for a Loop

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 Wing Span- 24” (both wings) Wing Chord- 6” Wing Gap- 4.25” Wing Area- 288 sq. in (2 sq. ft) Fuselage ” Tail span- 14” Tail Chord- 4.5” Tail Arm ” Max AUW- 860 gm (30.27 oz) Wing loading oz/sq. ft

Videography Platform

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

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

CASDE MAV Configuration Fixed Wing with Speed of Metres/Sec. Avionics Payload of ~ 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

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

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’ Weight % 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

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