You are leading the testing effort for a system that controls the air/fuel ratio of direct-injection fuel devices designed specifically for high-altitude rescue helicopter engines. At altitude, the system must perform sufficiently to make enough air/fuel ratio adjustments per millisecond between fuel and both an on-board source and available ambient air, so as to prevent an engine stall caused by oxygen starvation. The system follows a sequential development lifecycle.
For this safety-critical software, at what appropriate point in the lifecycle should the performance goals be identified and defined?
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