Effect of nose-mounted control-system jets in roll-control positions on the aerodynamics of a space vehicle
Nose-mounted control-system jets in roll-control positions effect on aerodynamics of space vehicle
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Nose-mounted control-system jets in roll-control positions effect on aerodynamics of space vehicle
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ram-pressure jet controls on ring tail
Transonic wind tunnel study of control span and large wing-tip nacelles results on effectiveness of spoiler-slot-deflector controls on fighter aircraft
Effect of body nose blunting, control planform area, and leading edge bluntness on aerodynamic control of semivertex cone at hypersonic speed
Two axis compensatory manual control systems with compatible integrated display and control
Linear and nonlinear control systems via state variable feedback with applications in nuclear reactor control
Measurement and display of control information using remote manipulation and manual control techniques
Human controller behavior in multivariable control systems
Control of water moderated nuclear reactor using neutron absorbing helium 3 gas control elements
High accuracy feedback control systems might employ tiers of actuators with different properties. Such systems performance can be estimated in advance using Bode integrals. The systems can be made globally stable with good transient responses and close to the best possible disturbance rejection when controllers include high-order linear links and multiple nonlinear dynamic links. The design approach is exemplified by designing conb-ol system for an interferometer optical delay line.
A study of conceptual integration and performance aspects of localized active flow control (AFC) technology onto wings of short-to-medium-range project passenger airplanes is summarized. Using predicted aerodynamic performance improvement opportunities on the CFD Reference Aircraft, estimated benefit opportunities for conceptual implementation of studied wing localized active flow control (AFC) technology for low-speed (take-off and landing) application on a Performance Reference Aircraft configuration are presented. Using conceptual AFC systems and structural integration weight penalties for studied concepts, potential relevant net performance benefits can be obtained with reliable AFC in takeoff and landing. The conceptual integration study identifies potential promising localized wing AFC application opportunities for high-lift conditions using energy sources for modern aircraft. Material benefits are estimated for take-off and landing configurations for selected localized AFC applications. Next steps to refine and expand results of investigated topics, as well as possible other local AFC wing applications, are suggested.
This document is the final technical report for the UC Davis project DE-SC00023500, detailing the development and implementation of a Fast Recurrent Neural Network (FRNN) software. The software was designed to enable predictive, real-time control of plasma instabilities within the DIII-D Plasma Control System (PCS).
Control trailing-edge thickness and aspect ratio effect on oscillating hinge-moment and flutter characteristics of flap-type controls
Capability of lateral control system to provide aerodynamic heading-angle control of vehicle having maximum lift-drag ratio during reentry
Motion stabilization of controlled member in control system with time delay
Application and extension of modern automatic control theory to nuclear rocket dynamics and control
Liapunov method for closed loop time optimal control of linear systems with bounded control norm using eigenvector scalar product solution for Hamilton-Jacobi equation
Charge-current control circuit for nickel-cadmium cells with control electrodes