Решение задачи ориентации для беспилотных летательных аппаратов

Abstract

The article describes the range of aircraft location vertical finders to determine the pitch and roll angles. The mentioned devices reflect the main stages of the attitude control system development throughout the history at the Control Device Depart- ment of the Tula State University, ranging from classical platform systems to mi- cromechanical and pyrometer strapdown attitude reference systems. A multifunctional attitude gyroscope based on two two-degree-of-freedom gyros driven by electric gyro motors has been discussed as a classical platform attitude gyroscope. Strapdown vertical references are represented by system samples based on micro- mechanical inertial sensors and pyrometer detectors. The article provides the specifications of the vertical references concerned and performs the comparative analysis thereof. It also shows the advantages and disadvantages of each of these systems.