Title
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations: A Generic Approach from Subsonic to H,Used
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This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static, dynamic, and maneuver stability requirements, while taking the sixdegreeoffreedom trim state into account. The stability and control analysis solves the static and dynamic equations of motion combined with nonlinear vortex lattice aerodynamics for analysis.The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably wellknown symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineeringscientific method itself is derived throughout the second half of the book.This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a configuration stability & control methodology module for an advanced multidisciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
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This product may contain chemicals known to the State of California to cause cancer, birth defects, or other reproductive harm.
For more information, please visit www.P65Warnings.ca.gov.