title: ÐÐ¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ Ð´Ð°ÑÑÐ¸ÐºÐ¾Ð² Ð±ÐµÑÐ¿Ð¸Ð»Ð¾ÑÐ½Ð¾Ð³Ð¾ Ð»ÐµÑÐ°ÑÐµÐ»ÑÐ½Ð¾Ð³Ð¾ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ° Ð´Ð»Ñ ÑÐ¾ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð½Ð°Ð±Ð¾ÑÐ° Ð´Ð°Ð½Ð½ÑÑ Ð¸Ð¼Ð¸ÑÐ°ÑÐ¸Ð¾Ð½Ð½ÑÑ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ¾Ð² Ð´Ð»Ñ Ð¾ÑÐµÐ½ÐºÐ¸ Ð°Ð»Ð³Ð¾ÑÐ¸ÑÐ¼Ð¾Ð² Ð¾Ð¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ð¸Ñ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸
title: Modeling sensors of UAV for generating dataset of simulated experiments to evaluate algorithms of attitude estimation
Creators: name: ÐÑÑÐ°Ð´, ÐÐ¼Ð¼Ð°Ñ
name: Ð¡ÐµÑÐ¸ÐºÐ¾Ð², Ð¡ÐµÑÐ³ÐµÐ¹
name: "Ð¡Ð¾Ð²ÑÐµÐ¼ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð°ÑÐ¸Ð½Ð¾ÑÑÑÐ¾ÐµÐ½Ð¸Ðµ: Ð½Ð°ÑÐºÐ° Ð¸ Ð¾Ð±ÑÐ°Ð·Ð¾Ð²Ð°Ð½Ð¸Ðµ", Ð¼ÐµÐ¶Ð´ÑÐ½Ð°ÑÐ¾Ð´Ð½Ð°Ñ Ð½Ð°ÑÑÐ½Ð°Ñ ÐºÐ¾Ð½ÑÐµÑÐµÐ½ÑÐ¸Ñ (13; 2024; Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³)
Publisher: name: ÐÐÐÐÐ¢ÐÐ¥-ÐÐ ÐÐ¡Ð¡
Year: 2024
Subjects: ÐÐµÑÐ°ÑÐµÐ»ÑÐ½ÑÐµ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑ Ð±ÐµÑÐ¿Ð¸Ð»Ð¾ÑÐ½ÑÐµ
ÐÐ¸ÑÐ¾ÑÐºÐ¾Ð¿Ñ
ÐÐºÑÐµÐ»ÐµÑÐ¾Ð¼ÐµÑÑÑ
Ð¼Ð°Ð³Ð½ÐµÑÐ¾Ð¼ÐµÑÑÑ
ÑÐ³Ð»Ñ Ð­Ð¹Ð»ÐµÑÐ°
magnetometers
Euler angles

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description: This article illustrates a method for generating data that simulates Unmanned Aerial Vehicles (UAV) measurements for attitude estimation problems, the generated data contains measurement of Gyroscopes, Accelerometers and Magnetometers as sensors, it also contains the attitude data which represent the UAV orientation as Euler angles or Quaternion. Since many researchers ask for simulated trips of UAV to evaluate their algorithms before implementing them in real-time applications. This depends basically on understanding the mathematical model of sensors, the true and real measurement with the existence of noise. The generated data contains noises to simulate real trips with different flight modes as it will be explained in details later. Gyroscopes drifts and Accelerometers biases are also generated with noises. External forces are also considered in case of flight modes such as maneuvers and added to accelerometers to emulate real world trips.