The Integrated Actuation Package Approach to Primary Flight Control 920968

Renewed interest in the attributes of the More Electric Airplane (MEA) is accelerating the development of power-by-wire actuation systems to perform the critical function of primary flight control. The Integrated Actuation Package (IAP™), which utilizes an electric motor driven servopump to control actuator position, is presented within as a prospective candidate to fill this demanding role.
Also presented is a design and performance overview of a dual channel IAP™ produced for flight test evaluation on the Lockheed High Technology Test Bed (HTTB).


Subscribers can view annotate, and download all of SAE's content. Learn More »


Members save up to 43% off list price.
Login to see discount.
Special Offer: With TechSelect, you decide what SAE Technical Papers you need, when you need them, and how much you want to pay.