Industrial Automatic Control Systems and Controllers Annotation << Back Technological Stand for Debugging Software and Mathematical Support and Control of Technical Characteristics of Inertial Navigation Systems of Aircraft. Universal Test Equipment for Onboard Systems O.V. Skudneva The article discusses the development of the laboratory installation for debugging software and control the technical characteristics of inertial navigation systems, manned and unmanned aerial vehicles through the use of a real inertial system, a personal computer, standard and special devices. It shows the structural-functional scheme of the laboratory installation. It defines the composition, function and technical features included in the stand devices. A short reference is given to the technical characteristics of the inertial system and frame mounting structures and control and rotary table, designed for the installation of a monoblock, adjusting and setting angles. It shows the front panel of the power supply connection on the wiring indicating the destination of incoming controls and pin assignments for wiring. The structure of the device for control and debugging software inertial navigation system is based on personal computer bus with ISA installed in his channels of communication. The technical proposals to create universal checkout equipment to control onboard instrumentation of other types of systems and complexes is given. Materials of the article are designed to develop methodological materials for training the students to work with a real inertial navigation system and control and test equipment consisting of laboratory bench. Also, the article may be useful for developers and operators, flight-navigation equipment of aircraft specialusts. Keywords: aircraft; inertial system; inertial navigation system; software and mathematical support; control and testing equipment; Personal Computer; power panel; control panel. DOI: 10.25791/asu.10.2020.1222 Pp. 03-11.