Збруцький О.В.

A concept has been developed for the creation of a small-sized universal base chassis of a robot of high cross-country ability and maneuverability, which combines minimization of the dimensions and weight of mobile robots, a reduction in production costs due to a decrease in resource and material consumption, a significant expansion of the scope of use of mobile robots in areas where traditional large-sized equipment cannot be applied , the implementation of which is based on the use of chassis kinematic schemes, providing high cross-country ability on rough terrain and in houses with the a

Modern complex control algorithms for group of unmanned aerial vehicles (UAVs) are developed. Developed and implemented a control system for the integrated use of UAVs group through the use of machine vision systems. Worked out algorithms and guidance system means that are installed on board of each UAV. Proposed system calculates the spatial position of the leading UAV, that are converted into command signals for characterization end estimation of the changing in the spatial position of the leading UAV.

A new principle of attitude control system of ultra-small spacecraft (SKA) is developed, which is based on the determination of the spatial orientation of SKA by information of multi-antenna GPS-system and further usage of this information in the control loop of engine-flywheel (EF) - executing element of control system of angular motion of SKA. Methods and algorithms for determining the spatial orientation of SKA are investigated, as well as methods and algorithms for signal generation of the angular acceleration, which will significantly expand the resources of the precision of EF.

Design of thin-walled metal tubes are becoming more common in the construction of modern light aircraft, both manned and unmanned due to its exceptional workability, durability and long service life.

The work is dedicated to the development and implementation of integrated design methodologies of individual elements of unmanned aircraft systems related to the problems of ensuring the necessary tactical and technical, performance, reliability characteristics, performance and unification into a single unified methodology and a system of making design decisions in the design process.

Analyzed the causes of abnormal and dangerous situation in the operation of unmanned aircraft and general purpose aircraft, manned by a single pilot. It is possible to determine the number of events that will lead to a decrease in dangerous situations during the flight of the aircraft: carrying out timely maintenance and monitoring of the physical and psychological integrity of the pilot at his control of the aircraft, correct and timely assessment of the weather conditions, applying for aircraft auxiliary / reserving devices and systems.

Bases of creation of midget space vehicles  as space microlaboratories are worked out. Theoretical and experimental researches are conducted on creation of the systems of microsatellites, basic scheme-technical decisions are worked out, software is developed. The ground center of communication with microsatellites in the amateur range of frequencies for realization of space experiments is created