发明名称 |
STALL, BUFFETING, LOW SPEED AND HIGH ATTITUDE PROTECTION SYSTEM |
摘要 |
A flight control system moves elevators according to a pilot command summed with an automatic command. The flight control system monitors a set of flight parameters to determine if the flight vehicle is operating inside a permitted envelope. The flight controls system incorporates automatic protections thru the automatic elevator command if the flight vehicle is close to its envelope limits. The exemplary illustrative non-limiting implementation herein provides automatic protections in order to protect the flight vehicle from low speeds, high attitude, stalls and buffetings.
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申请公布号 |
US2009062973(A1) |
申请公布日期 |
2009.03.05 |
申请号 |
US20070849501 |
申请日期 |
2007.09.04 |
申请人 |
CALDEIRA FABRICIO REIS;GANGSAAS DAGFINN;POLATI DE SOUZA ALVARO VITOR;DA SILVA MARTINS EDUARDO;SGUERRA VITA MARCO TULIO;FILHO JOSE MARCIO VIEIRA DIAS;CAMPOS MARCOS VINICIUS;FREITAS EMERSON |
发明人 |
CALDEIRA FABRICIO REIS;GANGSAAS DAGFINN;POLATI DE SOUZA ALVARO VITOR;DA SILVA MARTINS EDUARDO;SGUERRA VITA MARCO TULIO;FILHO JOSE MARCIO VIEIRA DIAS;CAMPOS MARCOS VINICIUS;FREITAS EMERSON |
分类号 |
G05D1/08;G06F7/00;G06F17/00 |
主分类号 |
G05D1/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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