Andere Kunden interessierten sich auch für
![Development of Experimental, Analytical, and Numerical Approximations Appropriate for Nonlinear Damping Coatings]( "Development of Experimental, Analytical, and Numerical Approximations Appropriate for Nonlinear Damping Coatings")
Development of Experimental, Analytical, and Numerical Approximations Appropriate for Nonlinear Damping Coatings60,99 €![Evaluation of Factors Contributing to Damping of Coated and Uncoated Titanium Plates]( "Evaluation of Factors Contributing to Damping of Coated and Uncoated Titanium Plates")
Evaluation of Factors Contributing to Damping of Coated and Uncoated Titanium Plates64,99 €![Anelastic Study of Divacancy Damping in Gold]( "Anelastic Study of Divacancy Damping in Gold")
Anelastic Study of Divacancy Damping in Gold61,99 €![Evaluation Techniques for Determining Damping Mechanisms on Titanium Plates]( "Evaluation Techniques for Determining Damping Mechanisms on Titanium Plates")
Evaluation Techniques for Determining Damping Mechanisms on Titanium Plates60,99 €![Student Support for Research in Hierarchical Control and Trajectory Planning]( "Student Support for Research in Hierarchical Control and Trajectory Planning")
Student Support for Research in Hierarchical Control and Trajectory Planning61,99 €![Optimal Sensor Threshold Control and the Weapon Operating Characteristic for Autonomous Search and Attack Munitions]( "Optimal Sensor Threshold Control and the Weapon Operating Characteristic for Autonomous Search and Attack Munitions")
Optimal Sensor Threshold Control and the Weapon Operating Characteristic for Autonomous Search and Attack Munitions60,99 €![The Longitudinal Effects of Self-Monitoring and Locus Of Control on Social Network Position in Friendship Networks]( "The Longitudinal Effects of Self-Monitoring and Locus Of Control on Social Network Position in Friendship Networks")
The Longitudinal Effects of Self-Monitoring and Locus Of Control on Social Network Position in Friendship Networks60,99 €
A novel phugoid damping control design methodology is developed, based on the use of wind axes and a point-mass aircraft model. The state variables are air speed, flight path angle, and heading angle, the control variables are thrust setting, angle of attack, bank angle, and sideslip angle, and the command signals are airspeed, flight path angle, and heading angle or heading rate. All the variables and parameters are nondimensionalized. A multivariable set point controller is developed which consists of: (i) a trim calculation-based nonlinear feed-forward control computer; thus, given a commanded new trim state (air speed, flight path angle, and yaw rate), the required trim thrust setting and trim angle of attack, bank angle, and sideslip angle inputs are determined, and, (ii) a small signal linear feedback regulator; the equations of motion linearized about the trim condition of wings level, and constant altitude flight, which simplifies the dynamics to allow separation between the lateral and longitudinal control channels, are used, and a small-signal linear multivariable regulator is designed. The linear compensator also entails integral action.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.