Lockheed Martin Challenge

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Presentation transcript:

Lockheed Martin Challenge Ron Lockheed Martin Challenge

Problem Statement Problem Statement   Current UAV technology is not capable of launching vertically using a rail launch system into the atmosphere.  As such, current UAV’s are not suitable for use for urban operations as they must be launched away from the urban setting due to obstacles. This presents problems for certain missions that could be assisted by UAV technology.   Ron

Operating Environment and Use Urban environment Heat Controlled by soldier with limited experience Fly autonomous and transmit video

System Block Diagram

Video Transmission System Last Year’s System: Transmitted on 2.4 GHz at 1 watt Could not reach the full 1 mile Highly prone to interference Did not meet FCC regulations for ATV Ron

Video Transmission System New System Choice of Frequency (440 Mhz): Choice of Transmitter (2 watt) Choice of Antenna Meeting FCC Regulations FCC allows transmit power of up to 50 watts on 440 MHz Ron

Video Transmission System Ron

Video Transmission System Plans for Testing: Test with just video transmitter and computer TV capture card Test with just video transmitter and down-converter Test with down-converter and IF converter Full system test: Range tests (transmitter and receiver placed at different distances) Interference tests (transmitter and receiver placed across buildings) Tests performed with various antenna design iterations Ron

Power System Last Year’s System: 1400 mAh NiCad Battery The DC‐DC converter is fed by the avionics battery and supplies appropriate voltages to on‐board avionics equipment (5V and 12V). 1400 mAh NiCad Battery Weight=156g+183g+30g=369g Approx run time=30 Minutes Ron

Power System New System Design: 2350 mAh 14.8V Lipoly Battery Two switching regulators are used to supply both 11V and 5V to the desired systems. 2350 mAh 14.8V Lipoly Battery Weight=262g+32g=294g Approx run time=2.15 Hours Ron

Autopilot

Autopilot

Autopilot

Resources and Schedule

Resources and Schedule

Questions

Lockheed Martin Corporation REPORT DISCLAIMER NOTICE DISCLAIMER: This document was developed as a part of the requirements of a multidisciplinary engineering course at Iowa State University, Ames, Iowa. This document does not constitute a professional engineering design or a professional land surveying document. Although the information is intended to be accurate, the associated students, faculty, and Iowa State University make no claims, promises, or guarantees about the accuracy, completeness, quality, or adequacy of the information. The user of this document shall ensure that any such use does not violate any laws with regard to professional licensing and certification requirements. This use includes any work resulting from this student-prepared document that is required to be under the responsible charge of a licensed engineer or surveyor. This document is copyrighted by the students who produced this document and the associated faculty advisors. No part may be reproduced without the written permission of the course coordinator. Images within this presentation were obtained via the courtesy of their respective owners, listed below: Lockheed Martin Corporation MicroPilot