Wednesday, May 6, 2020
A Real Time Computer System For A Passenger Plane Ã¢â¬ Free Samples
Question: Discuss about the Real Time Computer System For A Passenger Plane. Answer: Requirements of the organization: The passenger plane must use mainframe computers, as the mainframe computers are highly reliable. The mainframe computers are fast as the computer consists of large number of CPU, which powers the more processing power. These types of computers uses high memory, so that the entire system can be backup if any system crash is happen. Some safety measurements needs to be addressed on the computers that in case of any emergency, the passengers can communicate over the air with the nearest airport or they can send some emergency message by on click action using the computer. Robustness of the computer depends on the reliability, serviceability and on the availability measurement (Giselsson 2013). An investment is not an issue in the implementation of the real time computer system in the passenger plane. More the money spends more high will be the hardware and software features quality. the mainframe computers has the ability of time sharing that is in real time many people can use the mac hines simultaneously with high efficiency. The performances of the mainframe computers is high because this computer share the workload with the different processors and some devices, it also increases the processing ability of the computer that can be helpful for the computer system in the passenger plane. Type of the computer system proposed: The type of the computer system that is going to apply in the passenger plane must have some certain capabilities. The computer system must consist of a real time system, which can control the aircraft by itself. To control the flight by the computer system, an aircraft control system is going to be applied in the computer system. The computer system must consist of some subsystems that can control the mechanical system as well as the aerodynamics. An autopilot is a flight control system that allows the airplane to fly without the pilot (Kastner and Looye 2013). The pilot needs to set the mode they want in the autopilot either heading hold mode or altitude hold mode. The computer system must consists of a communication system by which the pilots can communicate with the co plot and the craft crew as well as the pilots can communicate with the air station via radio frequency. The computer system for the passenger also needs a communication system so that they can anytime communicate w ith the aircraft crew if the passenger needs any kind of help. The communication system can help in the emergency any people can send emergency message to the nearest aerostation possible so in the emergency to get any kind of help where time matters most (Khan, Tahir and Khan 2015). An entertainment system for the passenger is also needs to be implemented in the computer system as the passenger can get entertainment on their journey (Wolf, Minzlaff and Moser 2014). These all features enhance the aircraft and the main thing is the computer system by which these systems can be controlled and served for the passengers. Implementing this kind of aircraft needed huge investment so the updated system can be use to make the computer system on the passenger airplane. References: Giselsson, P., 2013, June. Output feedback distributed model predictive control with inherent robustness properties. InAmerican Control Conference (ACC), 2013(pp. 1691-1696). IEEE. Kastner, N. and Looye, G., 2013. Generic tecs based autopilot for an electric high altitude solar powered aircraft.CEAS EuroGNC. Delft, The Netherlands: CEAS, pp.10-12. Khan, F., Jan, S.R., Tahir, M. and Khan, S., 2015, October. Applications, limitations, and improvements in visible light communication systems. InConnected Vehicles and Expo (ICCVE), 2015 International Conference on(pp. 259-262). IEEE. Wolf, M., Minzlaff, M. and Moser, M., 2014. Information technology security threats to modern e-enabled aircraft: A cautionary note.Journal of Aerospace Information Systems,11(7), pp.447-457.