Design and Prognosis of CanSat Maneuver Systems Using Machine Learning
摘要
The CanSat uses an advanced ultra-light microcontroller, pressure and temperature sensors, a 3-axis accelerometer, a 3-axis gyro, a camera, GPS, an IR distance measuring sensor, and an RF communication module to communicate with a ground station PC. The design and navigation control of an advanced-level comeback CanSat, which is going to be launched to high altitude (between 2400 and 3658 m) using an amateur rocket from ground level, requires efficient control systems. In this paper, we present an advanced CanSat simulation and design methodology incorporating machine learning (ML) to enhance navigation, maneuverability, and resilience against sensor failures The simulation incorporates realistic sensor behaviors and malfunctions, such as gyroscopic drift, pressure sensor freezing, and temperature interference, enabling robust testing of ML-based solutions.