一个简短的起飞和着陆(短距起降)飞机必须能够控制飞行速度低,但它也必须接受上述报价越野(巡航)的性能。
A short take-off and landing (STOL) aircraft must be able to fly at low controlled speeds, yet it must also offer acceptable cross-country (cruise) performance.
所述车辆的速度可基于所述巡航控制指令来控制。
A speed of the vehicle can be controlled based on the cruise control commands.
经分析计算与试飞结果表明,对于爬升较缓慢的飞机,本控制方案可实现沿优化性能轨迹上升,并自动转入有利速度巡航。
It is shown that the climbing control plan is applicable to the aircraft with slower climbing according to optimum performance trajectory and automatically fly with optimum cruising velocity.
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