Your search result 8 registers
Aeronautical Systems: Dynamics and Control Thresholds for Gauss-Newton Optimization at Output-Error Method Applied for System Identification in Helicopter Flight Test Data Sérgio de Oliveira; Luciano Menegaldo, pages 1032-1038
Aeronautical Systems: Dynamics and Control Search Optimal Trajectories using EVGA and Solar Electric Propulsion Denilson Paulo Santos; Antonio Prado, pages 1039-1045
Aeronautical Systems: Dynamics and Control Análise de Robustez do Método Híbrido de Estimação de Dano Estrutural Leonardo Santos; Leonardo Chiwiacowsky; Haroldo Campos Velho, pages 1046-1051
Aeronautical Systems: Dynamics and Control The Influence of the Positive Pitch-Flap Coupling (Negative Delta3) on the Flapping Response of an Articulated Tail Rotor José Márcio Pereira Figueira; Ronaldo Cruz; Donizeti de Andrad, pages 1052-1059
Aeronautical Systems: Dynamics and Control Application of Predictive Control Techniques to a Helicopter Blade Sailing System Vinícius Piccirillo, pages 1060-1067
Aeronautical Systems: Dynamics and Control On the Air in Servo Valve Hydraulic Control Systems Carlos Corteline, pages 1068-1073
Aeronautical Systems: Dynamics and Control Aeroelastic Analisys of the Blade Sailing Phenomenon in Helicopters Under Magnetorheological-HystereticEffects Kleber Augusto Castão; Luiz Carlos Sandoval Goes; José M. Balthazar; Roberto Luiz da Cunha Barroso Ramos, pages 1074-1079
Aeronautical Systems: Dynamics and Control High Frequency Modeling of a Hydraulic Actuation Flight Control System Carlos Constantino; Luiz Carlos Sandoval Goes; Fernando Moreir, pages 1080-1090