A hardware/software architecture for UAV payload and mission control
This paper presents an embedded hardware/software architecture specially designed to be
applied on mini/micro unmanned aerial vehicles (UAV). An UAV is low-cost non-piloted
airplane designed to operate in D-cube (dangerous-dirty-dull) situations. Many types of
UAVs exist today; however with the advent of UAVs civil applications, the class of mini/micro
UAVs is emerging as a valid option in a commercial scenario. This type of UAV shares
limitations with most computer embedded systems: limited space, limited power resources …
applied on mini/micro unmanned aerial vehicles (UAV). An UAV is low-cost non-piloted
airplane designed to operate in D-cube (dangerous-dirty-dull) situations. Many types of
UAVs exist today; however with the advent of UAVs civil applications, the class of mini/micro
UAVs is emerging as a valid option in a commercial scenario. This type of UAV shares
limitations with most computer embedded systems: limited space, limited power resources …
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