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Avionics Practice Test: Avionics System Integration
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Avionics System Integration topics include: Data bus systems, modular avionics architectures and uav avionics. Avionics system integration is the process of combining and controlling smaller systems to form an overall system. It involves designing, installing, testing, and certifying electronic equipment and software.  Avionics systems are made up of many smaller sub-systems. The integrated avionics system's functions include: Establishing the IMA platform Sharing platform resources Providing system-hosted integrated programs Building system cross-linked networks Supporting the... Show more
Avionics Practice Test: Avionics System Integration
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25 Questions

1. In an aircraft, serial data transfer is achieved by _________
2. How are Data bus in avionics architecture broadly divided into?
3. What property does data transmission in fiber optic cable exploit?
4. A flight management system is not necessary for simple UAVs.
5. What is the cost-effective solution for UAV displays?
6. In an aircraft, serial data transfer is achieved by _________
7. What is the altitude of HALE?
8. Avionics Full Duplex Switched Ethernet provides flexibility to manage any change in the data communication between the connected systems without wiring modifications.
9. What is the altitude of HALE?
10. Which type of avionic architecture was the first to use DIAS?
11. Which type of avionic architecture was the first to use DIAS?
12. In a radio controlled UAV, FHSS technology has more advantage than DSSS technology.
13. What is the failure probability for a UAV?
14. What type of avionic architecture is used in the JSF?
15. Which one of the following is not true with respect with centralized architecture?
16. Which one of the following is not a true with respect to integrated modular avionics architecture?
17. The type of Ethernet data bus adapted for airborne applications is _______
18. A time shared multiplex highway is used in Federated avionic architecture.
19. The type of Ethernet data bus adapted for airborne applications is _______
20. Which one of the following is not true with respect with centralized architecture?
21. Avionics Full Duplex Switched Ethernet provides flexibility to manage any change in the data communication between the connected systems without wiring modifications.
22. A flight management system is not necessary for simple UAVs.
23. Which of the following is false with respect to AIRNIC?
24. What type of cable does MIL STD 1553 use?
25. The architecture where each component had its own sensors, processing and display is called as ________

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