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Question 1: What is the role of hardware-in-the-loop (HIL) testing in aerospace software development?

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Question 2: What method would you use to test the interoperability of aerospace software systems with external systems?

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Question 3: When designing fault-tolerant embedded systems for aerospace applications, which redundancy method is most effective for mitigating hardware failures?

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Question 4: When simulating aircraft propulsion systems, which parameter is most critical for performance evaluation?

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Question 5: What is the impact of "Real-Time Software Constraints" on C/C++ programming in aerospace systems, and how do you ensure that your code meets these constraints?

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Question 6: How does "Data Link Communication" work in aerospace, and what role does software play in ensuring reliable communication between aircraft and ground stations?

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