An approach of solving the integrated automated test control systems (IATCS) tasks has been considered. The structure of IATCS, conditions of functioning, composition by the unity matrix, classification according to different criteria have been presented for understanding the system operation. It makes better to increase the level of automation as part of a complex system throughout the life cycle of aviation equipment
The aim is to develop the automatic control system which doesn't contain the transducer of position ...
During the operation of the machinery, units and blocks are constantly affected by a number of chara...
The system of technical operation (TO) of on-board equipment or avionics of aircraft (AC) as an obje...
This paper proposes a design and development of system integrated test facility for Integrated Archi...
Nowadays the development of aviation leads to the all-time increase of the air traffic density in th...
The system of operational control (SOC) of civil aircraft (CA) airborne equipment incorporates onboa...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The quality control system for an aircraft engine that is continuously developed in the life cycle s...
Avionics of the present day comprises advanced technology and software-intensive systems. Earlier ge...
The engineering and fabrication of the test ACT system, produced in the third program element of the...
Fly-by-wire systems are becoming increasingly common in civil transport aircraft due to the economic...
International Telemetering Conference Proceedings / October 25-28, 1993 / Riviera Hotel and Conventi...
PDFTech ReportAD-A228 934Air traffic controlAirspace (Aeronautics)AvionicsCommunicationNavigationSur...
International Telemetering Conference Proceedings / October 09-11, 1973 / Sheraton Inn Northeast, Wa...
When developing a new aircraft, the airframer encounters various (partly contradictory) demands and ...
The aim is to develop the automatic control system which doesn't contain the transducer of position ...
During the operation of the machinery, units and blocks are constantly affected by a number of chara...
The system of technical operation (TO) of on-board equipment or avionics of aircraft (AC) as an obje...
This paper proposes a design and development of system integrated test facility for Integrated Archi...
Nowadays the development of aviation leads to the all-time increase of the air traffic density in th...
The system of operational control (SOC) of civil aircraft (CA) airborne equipment incorporates onboa...
An active controls technology (ACT) system architecture was selected based on current technology sys...
The quality control system for an aircraft engine that is continuously developed in the life cycle s...
Avionics of the present day comprises advanced technology and software-intensive systems. Earlier ge...
The engineering and fabrication of the test ACT system, produced in the third program element of the...
Fly-by-wire systems are becoming increasingly common in civil transport aircraft due to the economic...
International Telemetering Conference Proceedings / October 25-28, 1993 / Riviera Hotel and Conventi...
PDFTech ReportAD-A228 934Air traffic controlAirspace (Aeronautics)AvionicsCommunicationNavigationSur...
International Telemetering Conference Proceedings / October 09-11, 1973 / Sheraton Inn Northeast, Wa...
When developing a new aircraft, the airframer encounters various (partly contradictory) demands and ...
The aim is to develop the automatic control system which doesn't contain the transducer of position ...
During the operation of the machinery, units and blocks are constantly affected by a number of chara...
The system of technical operation (TO) of on-board equipment or avionics of aircraft (AC) as an obje...