Electronics & Information Technologies for Unmanned Aerial Systems

课程简介

/ Indicative Syllabus System Component, Electronic Device, and Radio Link Common system components of UAS: airframe, servo, propulsion system (motor, electronic speed controller (ESC), propeller), Li-po battery, radio transmitter and receiver, telemetry, ground control station (GCS), and the autopilot. Dynamic Modelling of Unmanned Aerial Vehicle Coordinate systems, kinematic model, dynamic model, propulsion system model, controller allocation model of UAS and model linearisation method. Flight Control Framework Cascade control structure, position control, attitude control, and control allocation for the low-level control of UAS. Path and Trajectory Planning Global path planning for UAS including search-based methods and sample-based methods. Local smooth trajectory generation methods. Autopilot System Integration and Flight Simulation Open-source flight controller; Flight simulation platform; Programming and hardware interface; Implementation of control and planning algorithms, Introduction to autonomous aerial robotic system. Mini UAS Flight Test Integrate the hardware and software; flight test in an indoor laboratory. -- 1 of 3 --

目标

To provide students with knowledge of electronics and information technologies for unmanned aerial vehicles (UAV) and unmanned aircraft systems (UAS).

先修要求

/ Co-requisite/ Exclusion Pre-requisite: AAE2005 Electrics and Electronic for Aeronautical Engineering

Teaching Pattern

Methodology 1. The teaching and learning methods include lectures/hands on sessions, assignments, test, project and examination. 2. The continuous