ENHANCEMENTS AND MODERN APPLICATIONS OF PID CONTROLLERS FOR SMALL AIRCRAFT AHRS PERFORMANCE IMPROVEMENT
Abstract. Traditional PID controllers remain widely used in embedded flight control and stabilization systems. However, in small aircraft Attitude and Heading Reference Systems (AHRS), classical PID approaches are insufficient under sensor noise, drift, vibration, and energy limitations typical for lightweight avionics platforms.This paper proposes a context-aware, risk-sensitive PID framework for AHRS modernization. The controller integrates […]
THE MATHEMATICAL AND SIMULINK MODELS FOR DETERMINING ATTITUDE OF AIRCRAFT USING MEMS SENSORS
Abstract. This paper analyses the features, types and principles of construction of miniature gyroscopes and accelerometers, as one of the main types of sensors of inertial measuring systems. An analysis is also being made of the possibilities and prospects for integrating magnetometers and GPS modules into inertial computing systems, which significantly improvers the performance of […]
THE APPLICATION OF MEMS TECHNOLOGY TO DETERMINE AN AIRCRAFT ORIENTATION
Abstract. This paper analyzes the features of MEMS and the possibility of their use to build AHRS with flexible parameters, with the aim of using them on unmanned aerial vehicles. It is shown that the correct use of newer versions of modern MEMS, which have 3-axis gyroscopes, accelerometers and magnetometers, can provide complete and accurate […]
THE APPLICATION OF MEMS TECHNOLOGY TO DETERMINE AN AIRCRAFT ORIENTATION
Abstract. This paper analyzes the features of MEMS and the possibility of their use to build AHRS with flexible parameters, with the aim of using them on unmanned aerial vehicles. It is shown that the correct use of newer versions of modern MEMS, which have 3-axis gyroscopes, accelerometers and magnetometers, can provide complete and accurate […]