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The optimal mathematical models with high accuracy describing the parameters of these sensors in the working temperature range have been developed. The circuit engineering and construction solutions as well as the algorithms and hardware and software, implementing the obtained mathematical models in the electronic means for the temperature measurement, have been developed.
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Reliable, accident-free operation of extra light aviation, drone aircraft, the parachute equipment for landing of people and loads, demands to increase an accuracy of determination of height for the purpose of their safe maneuvering, descent and landing. In the work the critical analysis of existing methods of the height measurement has been carried out for the purpose of defining the most accurate ones and the preference has been given to the barometric method. To decrease the measurement errors, the smart altimeter sensors (SAS) intellectual sensors have been developed, and on their basis the prototype of a barometric altimeter have been designed. In the course of computer modeling and prototyping it has been determined that in designing the altimeter it is necessary to use several SAS, and the accuracy of measurements is essentially affected by an arrangement of sensors on a flying object. The developed method of the height measurement using SAS includes the hardware-software compensation of the errors, caused by the atmospheric phenomena and aerodynamic parameters of the flying object design. The hardware - software for processing the measured data has been developed as well as the software for functioning of intelligent pressure sensor, automatic data processing and the information output to the altimeter display. The tests on the offered technique and hardware - software have been carried out in actual practice of operation. The developed altimeter has been installed on the equipment of a parachutist. In the test result it has been determined that the developed original method and the hardware - software permit to significantly decrease the errors of measurements, which do not exceed 1 meter while the airflow moving at speeds up to 8 meters per second 5 meters up to 70 meters per second
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The mathematical models and the software and hardware tools for the intellectual microprocessor monitoring systems (MMS) of precise thermal equipment have been developed as a result of modeling the thermal equipment functional working characteristics. It has been shown that the equipment with MMS, implementing the above indicated mathematical models, provides high technical and operating characteristics.
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The intellectual system and the electron components for its functioning, allowing the implementation of the innovative method of measuring the individual heat consumption, have been developed. For intellectual system realization the original construction-technological circuit, hardware and software solutions have been developed for the intellectual system electron components. The methods and the mathematical models for calculation of individual heat consumption have been determined and stipulated.
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