LEADER 04283nam  22006015  450 
001 9910337621403321
005 20200706055003.0
010   $a3-030-16856-5
024 7 $a10.1007/978-3-030-16856-8
035   $a(CKB)4100000008743040
035   $a(MiAaPQ)EBC5837808
035   $a(DE-He213)978-3-030-16856-8
035   $a(PPN)238486346
035   $a(EXLCZ)994100000008743040
100   $a20190723d2019      u|             0
101 0 $aeng
135   $aurcnu||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStability and Control of Conventional and Unconventional Aerospace Vehicle Configurations$b[electronic resource] $eA Generic Approach from Subsonic to Hypersonic Speeds /$fby Bernd Chudoba
205   $a1st ed. 2019.
210  1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2019.
215   $a1 online resource (418 pages)
225 1 $aSpringer Aerospace Technology,$x1869-1730
311   $a3-030-16855-7 
327   $aIntroduction and Objectives -- Generic Aircraft Design ? Knowledge Utilization -- Assessment of the Aircraft Conceptual Design Process -- Generic Characterisation of Aircraft ? Parameter Reduction Process -- ?AeroMech? ? Conception of a Generic Stability and Control Methodology -- AeroMech Feasibility -- Conclusions -- Appendices.
330   $aThis book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ?configuration stability & control? methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
410  0$aSpringer Aerospace Technology,$x1869-1730
606   $aAerospace engineering
606   $aAstronautics
606   $aVibration
606   $aDynamical systems
606   $aDynamics
606   $aEngineering design
606   $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050
606   $aVibration, Dynamical Systems, Control$3https://scigraph.springernature.com/ontologies/product-market-codes/T15036
606   $aEngineering Design$3https://scigraph.springernature.com/ontologies/product-market-codes/T17020
615  0$aAerospace engineering.
615  0$aAstronautics.
615  0$aVibration.
615  0$aDynamical systems.
615  0$aDynamics.
615  0$aEngineering design.
615 14$aAerospace Technology and Astronautics.
615 24$aVibration, Dynamical Systems, Control.
615 24$aEngineering Design.
676   $a629.13236
700   $aChudoba$b Bernd$4aut$4http://id.loc.gov/vocabulary/relators/aut$0897251
906   $aBOOK
912   $a9910337621403321
996   $aStability and Control of Conventional and Unconventional Aerospace Vehicle Configurations$92004563
997   $aUNINA