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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 a radio controlled UAV, FHSS technology has more advantage than DSSS technology.
2. Which one of the following is not true with respect with centralized architecture?
3. The type of Ethernet data bus adapted for airborne applications is _______
4. Which avionic architecture allows the existence of heavily armed single seat fighters with a variety of weapons?
5. Which one of the following is not a true with respect to integrated modular avionics architecture?
6. What is the cost-effective solution for UAV displays?
7. Which type of avionic architecture was the first to use DIAS?
8. What is the altitude of HALE?
9. Which one of the following is the major difference between single mode and multi mode fibers?
10. Which one of the following is false with respect to TRN?
11. What is the failure probability for a UAV?
12. What property does data transmission in fiber optic cable exploit?
13. Avionics Full Duplex Switched Ethernet provides flexibility to manage any change in the data communication between the connected systems without wiring modifications.
14. How are Data bus in avionics architecture broadly divided into?
15. What type of cable does MIL STD 1553 use?
16. What type of avionic architecture is used in the JSF?
17. What type of avionic architecture consist of a number of an interconnected but functionally independent subsystem with some degree of central computer of overall operating modes.
18. A flight management system is not necessary for simple UAVs.
19. What type of communication does the MQ-9 ‘reaper’ UCAV use?
20. The architecture where each component had its own sensors, processing and display is called as ________
21. Which of the following is false with respect to AIRNIC?
22. What is the fastest mode of data communication between components in aircraft?
23. In an aircraft, serial data transfer is achieved by _________
24. What advantage does the concept of IS2 add to the pave pace avionic architecture?
25. A time shared multiplex highway is used in Federated avionic architecture.

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