Designed for aerospace, electrical and control engineers, this volume covers such topics as techniques for aircraft conceptual design for mission performance and optimization of aerospace structures using mathematical functions for variable reduction.
Techniques for aircraft conceptual design for mission performance
comparing nonlinear multiobjective optimization methods, A.R. Dovi and G.A.
Wrenn; optimization of aero-space structures using mathematical functions for
variable reduction, U.L. Berkes; knowledge-based system techniques for pilot
aiding, H.H. Chin; techniques for optimal sensor placement for on-orbit model
identification and correlation of large aerospace system structures, D.C.
Kammer; investigation on the use of optimization techniques for helicopter
airframe vibrations design studies, T.S. Murthy; size-reduction techniques
for the determination of efficient aeroservoelastic models, M. Karpel;
sensitivity analysis of eigendata of aeroelastic systems, V.R. Murthy and Y.
Lu; a simplified general solution methodology for transient structural
dynamic problems with local nonlinearities, E.E. Henkel, et al; balanced
systems and structures - reduction, assignment and perturbations, W.
Gawronski; response-only measurement techniques for the determination of
aero-space system structural characteristics, A.C. Lee and J.H. Chen; krylov
vector methods for model reduction and control of flexible structures, T.J.
Su and R.R. Craig, Jr.; maneuvering target tracking - imaging and non-imaging
sensors, M. Mariton and D.D. Sworder.
