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• W1528046862 abstract "The purpose of this chapter is to introduce the technical community to some of the adaptive flight control mechanisims and structures which have either lead directly to or actually flown in various classes of missiles, munitions and uninhabited aircraft. Although many programs are not open for publication, glimpses of a select few have made it to the public arena at various levels. This chapter is centered on airing several supersystem-level advances to flight-proven missiles, munitions and UAVs. Toward that end, basic models were typically used to lay out proof-of-concept flight hardware which was then fabricated, bench and/or ground tested, and incorporated in flight vehicles. In the early years, the adaptive aircraft were often simply flown, just to prove the concept worked. More recently, aircraft using adaptive flight control mechanisms have been flown off against conventional benchmark aircraft so as to demonstrate systemic superiority, thereby proving that flight control systems employing adaptive aerostructures result in some combination of lower power consumption, higher bandwidth, reduction in total aircraft empty weight, greater flight speed, shock resistance, lower part count, lower cost etc. On several occasions, adaptive aerostructures have even been shown to be enabling; that is, the aircraft class would not be able to fly without them. Although adaptive materials have been known for more than 120 years, the Aerospace industry has only more recently become aware of their basic characteristics. Starting in the mid 1980's Ed Crawley's group at MIT laid the foundations of what would become an active and vibrant branch of aerospace technology. With simple experiments on bending and extension-twist coupled plates, this group demonstrated that airloads on aerodynamic surfaces could be actively manipulated by using conventionally attached piezoelectric actuators.1-3 Although the structures resulting from these projects were not incorporated in flightworthy aircraft, their significance cannot be overstated as they introduced the technical community to the possibility of aircraft flight control with adaptive aerostructures and by doing so effectively started the entire field. Table 1 summarizes a collection of programs which have lead directly to a series of flight proven adaptive subscale aerospace systems." @default.
• W1528046862 created "2016-06-24" @default.
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• W1528046862 date "2011-04-11" @default.
• W1528046862 modified "2023-10-02" @default.
• W1528046862 title "Adaptive Fight Control Actuators and Mechanisms for Missiles, Munitions and Uninhabited Aerial Vehicles (UAVs)" @default.
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• W1528046862 doi "https://doi.org/10.5772/13796" @default.
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