COMBINED SYSTEM OF AUTONOMOUS CONTROL AND ORIENTATION OF MOVEMENT OF THE OBJECT IN 3D SPACE
DOI:
https://doi.org/10.34185/1562-9945-4-141-2022-04Keywords:
automatic control systems, aircraft, suborbital rocket, optical sensors, microcontroller, iner-tial systems, software algorithmsAbstract
The paper presents an analysis of the developments of the "Rocketry Agency Student Rock-et" project and identifies the main research directions for the development of this project. Prospects for the development of a research student project are the task of developing sub-orbital rockets with a flight altitude of 80, 100 or more kilometers. Flights to such altitudes are impossible without the use of monitoring and control systems, so an essential and high-priority task is development of a flight monitoring and control system for suborbital rockets with taking into account the caliber of the D-150 and D-300 launch vehicles. The analysis of modern monitoring and control systems has been carried out, the advantages and disad-vantages of these systems have been determined. The most attractive for use for suborbital rockets with the given caliber are autonomous guidance and television guidance systems. It is determined that the use of such control systems is impossible, both in terms of the di-mensions of the design itself, and the price category of the system as a whole. A new com-bined system of autonomous control and orientation of movement of volume in space, which is built on a combination of capabilities of television, inertial and mechanical systems, has been developed. regarding the determination and maintenance of the main vertical of the flight path of a suborbital rocket with a given caliber of the D-150 and D-300 launch vehicles.
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