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.
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
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