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Hardware Design of a Small UAV Flight Control System
Author(s): 
Pages: 64-67
Year: Issue:  9
Journal: Ordnance Industry Automation

Keyword:  UAVflight control system;
Abstract: For the disadvantage of traditional flight control computer system with single chip, design the flight control computer system of a small UAV. Technical index and functional is formulated, and TMS320F28335 chip is used as the core controller, which integrates GPS and sensor, and expands a few of communication interfaces. All of these designs ensure the real-time and reliability of data communication, and can achieve the independent autonomous navigation of small UAV. For the characteristics of low weight, small size and small power, the flight control system can provide a reference for the design and application of small UAV.
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