reduced order state-space
Full- & Reduced-Order State-Space Modeling of Wind Turbine Systems with Permanent Magnet Synchronous Generator
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EFFICIENT SCHEDULING OF WORKFLOW IN CLOUD ENVIORNMENT USING BILLING MODEL AWARE TASK CLUSTERING
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A Composite Robotic Controller Design Using Reduced Order Observer, Output Feedback and LQR and Its Application to Two Link Manipulator
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Reduced Order Modeling of the Pressure Distribution over the AGARD 445 6 Wing Read More: https://arc aiaa org/doi/abs/10 2514/6 2018 1760
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Traffic State Estimation via a Particle Filter Over a Reduced Measurement Space
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Abstract–– A Roll Position demand (as well as Roll Position Control) missile autopilot design methodology for a class of guided missile, based on state feedback, Ackermann pole-placement and reduced order Das & Ghosal observer (DGO), is proposed. The open loop unstable model of the roll control (or roll position demand) autopilot has been stabilized by using pole placement and state feedback. The non-minimum phase feature of rear controlled missile airframes is analyzed. Actuator dynamics has also been included in this design to make the overall system practically suitable for use. The overall responses of the Roll Control autopilot has been significantly improved over the frequency domain design approach where phase lag & phase lead compensator were used. Closed loop system poles are selected on the basis of desired time domain performance specifications. This set of roots not only to ensure the system damping, but also to make sure that the system can be fast. Reduced order Das & Ghosal (DGO) observer is implemented successfully in this design to estimate the Aileron angle and its rate. Finally a numerical example is considered and the simulated results are discussed in details. The date set has been chosen here for which largest rolling moment would occur (at Mach No = 4) due to unequal incidence in pitch and yaw.
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State-of-Charge Estimation of Lithium-ion Battery Based on a Novel Reduced Order Electrochemical Model
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Robust Fixed-order Gain-scheduling Autopilot Design using State-space Stability-Preserving Interpolation
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Exogenous expectations on endogenous uncertainty: recursive equilibrium and survival
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A Detailed Comparative Study between Reduced Order Cumming Observer & Reduced Order Das &Ghoshal Observer
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Abstract–– A flight path rate demand modified two-loop lateral missile autopilot design methodology for a class of rear controlled guided missile, based on state feedback, output feedback, reduced order Das & Ghosal observer (DGO) and PI controller is proposed. The open loop undamped model of two-loop autopilot has been stabilized by using pole placement and state feedback. The non-minimum phase feature of rear controlled missile airframes is analyzed. An optimal pole placement has been done through an iterative method such that the adverse effect of non-minimum phase property on the response of missile autopilot can be reduced considerably and also the system stability can be made better. The overall response of the modified two-loop autopilot has been significantly improved over the previous ones - specially the flight path rate and body rate. The flight path rate (as well as the lateral acceleration) has reached the commanded unit step input without compromising on its settling time thus it has been able to eliminate the steady state error. The system can now also cop up with the body rate demand and even the Maximum body rate demand is decreased to a great extent as compared to the classical two-loop design. Reduced order Das & Ghosal observer (DGO), using Generalized Matrix Inverse) is implemented successfully in this design. A program has been developed to find out the optimal pole positions and feedback gains according to the desired time domain performance specifications. Finally a numerical example has been considered and the simulated results are discussed in details.
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Computing inferences for large-scale continuous-time Markov chains by combining lumping with imprecision
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Reduced Order Modeling for Virtual Building Commissioning
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A canonical space-time state space model: state and parameter estimation
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Efficient Probabilistic Soil-Structure Interaction Analysis for Nuclear Structures Using A Fast Reduced Order Modeling in Probabilistic Space (ROMPS)
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Non-reduced rings of small order and their maximal graph
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Reinforcement learning for robot navigation in constrained environments
130
Reduced order based compensator control of thin film growth in a CVD reactor
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Reduced Order Models for Open Quantum Systems
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Sampled-data and reduced order controller implementation
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