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METHOD AND APPARATUS FOR PROTECTING AIRCRAFT MAXIMUM LIFT CAPABILITY
METHOD AND APPARATUS FOR PROTECTING AIRCRAFT MAXIMUM LIFT CAPABILITY
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机译:保护飞机最大举升能力的方法和装置
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摘要
An aircraft automatic control system protects structural parameters of an aircraft based on angle of attack protection by use of maximum allowed angle of attack values as a function of dynamic pressure or a combination of parameters that permit computation of dynamic pressure. Example techniques herein limit the wing lift coefficient as a function of dynamic pressure (or velocity) to create a limitation for the maximum lift produced by an aircraft wing.
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