A real time control algorithm for fixed-wing uavs in twin-boom inverted V-tail configuration
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Thông tin tài liệu:
In this paper, we propose a model of a real-time control algorithm for a fixed-wing uav in inverted v-tail configuration, including automatic takeoff phase, waypoint tracking phase and auto-landing phase.
Nội dung trích xuất từ tài liệu:
A real time control algorithm for fixed-wing uavs in twin-boom inverted V-tail configuration
Nội dung trích xuất từ tài liệu:
A real time control algorithm for fixed-wing uavs in twin-boom inverted V-tail configuration
Tìm kiếm theo từ khóa liên quan:
Inverted V-tail Fixed-wing Autonomous control PID controller Waypoint tracking phase Auto-landing phaseGợi ý tài liệu liên quan:
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