This thesis focuses on the design and implementation of a flight control system for a mini unmanned helicopter.
本文围绕超小型无人直升机飞行控制系统的设计与实现展开论述。
Because these wind loads are a major structural consideration, they greatly influence the design of the flight control system.
因为这些风载荷是结构上主要的考虑因素,它们很大地影响着飞行控制系统的设计。
ALTITUDE ACQUIRE, a digital flight control system mode to transition from climb (or descend) to level flight.
高度截获,一种数字式飞行操纵系统,从爬升(或下降)改平的模式。
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