| 摘要 |
A relatively simple system for avoiding light aircraft crashes, using rate-of-turn sensors, high pressure air containers and solenoid-operated air valves. The rate-of-turn sensors, when magnitude of turns exceed the predetermined values, close one or more relays, which then cause solenoids to operate to open air valves, allowing high pressure air to blast out to prevent misbehavior of the aircraft, such as excessive roll or pitch axis turning, while also providing buoyancy to the aircraft so that the aircraft does not lose altitude rapidly. This aircraft crash avoidance system operates automatically, without any need for pilot input. However, the pilot has the ability and option to disengage any or all portions of the crash avoidance system.
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