Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2005: Vol 219 Index PDF
Preview Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2005: Vol 219 Index
Author Index 2005 Allen, J I Aeronautics- 1903; aerospace-2003; ? ? 2103 Azzam, H Intelligent management of helicopter health and usage management systems data Balakrishnan, S N Midcourse guidance law with neural networks Belo, EM \ flutter suppression active controller Bornengo, D Evaluation of hexagonal chiral structure for morphing airfoil concept Bradley, R Quantification and prediction of pilot workload in the helicopter/ship dynamic interface Bruyere, | Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile Buggy, T W Quantification and prediction of pilot workload in the helicopter/ship dynamic interface Chakraborty, D Numerical investigation of transverse sonic injection in a non-reacting supersonic combustor Cook, J Intelligent management of helicopter health and usage management systems data Corchero, G An approach to the use of hydrogen for commercial aircraft engines Coton, | 4 simulation study of helicopter ship landing procedures incorporating measured flow-field data Cottrell, RG Minimizing manoeuvre advantage requirements for a hit-to-kill interceptor Davis, R N Autonomous component health management with failed component detection, identification, and avoidance De Marqui, C Jr \ flutter suppression active controller Farhadi, M Chree-dimensional study of separated flow over a square cylinder by large eddy simulation Franchini, S On the aerodynamics of leading-edge high-lift devices of avian wings Galbraith, R \ simulation study of helicopter ship landing procedures incorporating measured flow-field data Gill, | Prediction of stress concentrations associated with interacting stress-raisers within aircraft design: methodology development and application Golan, O M End-game guidance laws for dual-control missiles Graham, R H Prediction of stress concentrations associated with interacting stress-raisers within aircraft design: methodology development and application Grevtsov, N An application of the mechanical rotation scheme to an analysis of the motion of flying objects Gurfil, P Non-linear missile guidance synthesis using control Lyapunov functions Han, D Midcourse guidance law with neural networks Hess, RA Design and evaluation of a damage-tolerant flight control system Hong, YS Finite element analysis of shafts under combined loads Horn, J | Simulation of pilot workload for a helicopter operating in a turbulent ship airwake Hyde, T H Finite element analysis of shafts under combined loads Hyung, S Reconfigurable flight control system design using input-output information Kaderbek, D Pulse width modulating low power magnetic torquers for precise spacecraft attitude stabilization Kim, Y Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault Reconfigurable flight control system design using input-output information Knight, P Intelligent management of helicopter health and usage management systems data La Rosa, G Preliminary design and wind tunnel tests of a micro air vehicle for surveillance and sensor-bearing applications Léchevin N A multi-objective control approach for the synthesis of robust digital guidance laws 89 Lee, D Simulation of pilot workload for a helicopter operating in a turbulent ship airwake 145 Lee, DG Active homing performance enhancement with multiple model radome slope estimation 217 Lianos, D P Effect of sliding mode observers in the homing guidance loop 103 Long, L N Computational fluid dynamics simulations of ship airwake 369 Macdonald, C A Quantification and prediction of pilot workload in the helicopter/ship dynamic interface 429 Manna, P Numerical investigation of transverse sonic injection in a non-reacting supersonic combustor 205 Marques, F D A flutter suppression active controller 19 Melts, I An application of the mechanical rotation scheme to an analysis of the motion of flying objects 69 Meseguer, J On the aerodynamics of leading-edge high-lift devices of avian wings 63 © IMechE 2005 Proc. IMechE Vol. 219 Part G: J. Aerospace Engineering Author Index 2005 Mirone, G Preliminary design and wind tunnel tests of a micro air vehicle for surveillance and sensor-bearing applications Moghaddam, MM __ Robust, maneuvering control design of an aircraft via dynamic inversion and u-synthesis Montanes J | \n approach to the use of hydrogen for commercial aircraft engines Moon, G Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault Moosavi, S | Robust, maneuvering control design of an aircraft via dynamic inversion and p-synthesis Morgan, R W Minimizing manoeuvre advantage requirements for a hit-to-kill interceptor Nelson, E B Reconfigurable flight control Neville, 1 Dynamic and aerodynamic clearance of the Apache AH Mk] attack helicopter for embarked operations Newman, S Shipborne aviation: an introduction Ochi, Y Flight control system design for propulsion-controlled aircraft Ohlimeyer, E J Midcourse guidance law with neural networks Pachter, M Reconfigurable flight control Pérez-Grande | On the aerodynamics of leading-edge high-lift devices of avian wings Polites, M Pulse width modulating low power magnetic torquers for precise spacecraft attitude stabilization Polites, M | \utonomous component health management with failed component detection, identification, and avoidance Quarles, ( Pulse width modulating low power magnetic torquers for precise spacecraft attitude stabilization Rabbath, C A \ multi-objective control approach for the synthesis of robust digital guidance laws Rahnama, M lhree-dimensional study of separated flow over a square cylinder by large eddy simulation Raines, M Prediction of stress concentrations associated with interacting stress-raisers within aircraft design: methodology development and application Remillat, ( Evaluation of hexagonal chiral structure for morphing airfoil concept Risitano, A Preliminary design and wind tunnel tests of a micro air vehicle for surveillance and sensor-bearing applications Robotham, W S Finite element analysis of shafts under combined loads Sanz, J | On the aerodynamics of leading-edge high-lift devices of avian wings Sazonov, D \n application of the mechanical rotation scheme to an analysis of the motion of flying objects Scarpa, I Evaluation of hexagonal chiral structure for morphing airfoil concept Sezer-Uzol, N Computational fluid dynamics simulations of ship airwake Sharma, A Computational fluid dynamics simulations of ship airwake Shima, 1 End-game guidance laws for dual-control missiles Shin, D Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault Shin, S J Active homing performance enhancement with multiple model radome slope estimation Shinar, J Improved estimation is a prerequisite for successful terminal guidance Shkolnikov, | A Effect of sliding mode observers in the homing guidance loop Shtessel, Y B Effect of sliding mode observers in the homing guidance loop Song, T | Active homing performance enhancement with multiple model radome slope estimation Steinberg, M Historical overview of research in reconfigurable flight control Swift, K G Prediction of stress concentrations associated with interacting stress-raisers within aircraft design: methodology development and application Thomson, D G \ simulation study of helicopter ship landing procedures incorporating measured flow-field data rrevino, L ¢ \utonomous component health management with failed component detection, identification, and avoidance lsourdos, A Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile ruretsky, \ Improved estimation is a prerequisite for successful terminal guidance Vetter, T K Design and evaluation of a damage-tolerant flight control system Vincent, T | Minimizing manoeuvre advantage requirements for a hit-to-kill interceptor Visser, H G Optimization of high angle-of-attack approach to landing trajectories Wagstaff, P \n application of the mechanical rotation scheme to an analysis of the motion of flying objects Wells, S R Design and evaluation of a damage-tolerant flight control system White, B A Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile Williams, E J Finite element analysis of shafts under combined loads Zan, S J On aerodynamic modelling and simulation of the dynamic interface Proc. IMechE Vol. 219 Part G: J. Aerospace Engineering © IMechE 2005 = * # A - £ ‘ x ' > £ F € % @ : , .
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