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3 edition of Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1 found in the catalog.

Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1

Juan Salas InМѓigo

Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1

by Juan Salas InМѓigo

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  • 25 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Hypersonic planes.

  • Edition Notes

    StatementJuan Salas, T. Alan Lovell, and David K. Schmidt.
    SeriesNASA contractor report -- 192710., NASA contractor report -- NASA CR-192710.
    ContributionsLovell, T. Alan., Schmidt, D. K., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17681118M

    Published in: Proceeding: ACC'09 Proceedings of the conference on American Control Conference Pages St. Louis, Missouri, USA — June 10 - 12, Cited by: Full text of "Alternate Space Shuttle Concepts 3: Engineering and development plan. Volume 2: Orbiter vehicle" See other formats.

    AIAA Excel/VBA for Numerical Methods Education, Calculations and Applications in Energy Engineering Development of an Airframe-Propulsion Integrated Generic Hypersonic Vehicle Model (AIAA ) Clark, A. / Wu, Aerodynamic Shape Optimization of Hypersonic Vehicles (AIAA ) Kinney.   AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, Florida., January 08‐12, Details The AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference provides a unique forum dedicated to the latest developments in the collective disciplines of structures, structural dynamics.

    تحميل ():: Development of an Integrated Process, Modeling and Simulation Platform for Performance-Based Design of Low-Energy and High IEQ Buildings رسالة دكتوراه تحميل ():: Champs-Multizone and Virtual Building for Integrated Building Systems Design and Performance Evaluationرسالة دكتوراه. This chapter continues the presentation of a new parallel computational fluid dynamics (CFD) algorithm on unstructured grids. The chapter demonstrates the code's ability to solve the 3-D Navier-Stokes equations. The 2-D and 3-D results presented show excellent performance both .


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Development of a non-linear simulation for generic hypersonic vehicles -ASUHS1 by Juan Salas InМѓigo Download PDF EPUB FB2

The hypersonic vehicle, simulation results for the full nonlinear model with temperature variations and exogenous disturbances illustrate the boundedness of the controller with Table A Pitch rate, time to steady-state, used to generate Figure and (Part. A combined analytic and CFD-based two-dimensional airbreathing generic hypersonic flight vehicle model has been developed for control design and flight simulation environment.

[8] M. Bolender and D. Doman, “A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle,” in Proc.

AIAA Guid. Navig. Control Conf.,San Francisco, CA, Aug. [9] ––, “Modeling unsteady heating effects on the strucutral dynamics of a hypersonic. GNC Adaptive Flight Control and Fuzzy Logic • Wednesday, 17 August • hrs. A Simulation Environment for Testing and Research of Neurally Augmented Fault Tolerant Control Laws Based on Non-Linear Dynamic Inversion.

Mario Perhinschi, Marcello Simulation Software Development I • Monday, 16 August • hrs Six-DOF Modeling and Simulation of a Generic Hypersonic Vehicle for Conceptual Design Studies. () Polytopic linear parameter varying model-based tube model predictive control for hypersonic vehicles.

International Journal of Advanced Robotic Systems() Tensor-based ultrasonic data analysis for defect detection in fiber reinforced polymer (FRP) by: The effect of thermal and chemical boundary conditions on the structure and chemical composition of the wake behind a 3D Mach 7 sphere-cone at an angle of attack of 5 degrees and an altitude of roug m is explored.

A special emphasis is placed on determining the number density of chemical species which might lead to detection via the electromagnetic by: 1. An additional topic of interest covered in this Special Issue is the use of computational tools in aerodynamics and aeroelastic predictions.

The problem with these applications is the computational cost involved, particularly if this is viewed as a brute force calculation of a vehicle’s aerodynamics and structure responses through its flight : Mehdi Ghoreyshi.

This book provides a rigorous treatment of the fundamental concepts and techniques involved in process modeling and simulation. The book allows the reader to: (i) Get a solid grasp of “under-the-hood” mathematical results (ii) Develop models of sophisticated processes (iii) Transform models to different geometries and domains as appropriate.

Modeling and Simulation Tools for Heavy Lift Airships Ron Hochstetler SAIC Washington, DC non-linear flight dynamics simulation model for the YEZ-2A airship. While the model used wind tunnel data for the operational models are not only critical to the development of LTA. The system modeling and controller design for air-breathing hypersonic vehicles have always been one of the most highly challenging tasks to the development of hypersonic flight technologies due.

This paper studies the anti-disturbance control problem for air-breathing hypersonic vehicles (AHVs) with flexible dynamics and parameter uncertainties. A novel anti-disturbance control method is presented, which includes a robust coupling observer (RCO) and a linear quadratic regulator (LQR).Author: Na Wang, Lin Zhao, Chong Lin, Yumei Ma.

Automatic Control in Aerospace Selected Papers from the 12th IFAC Symposium, Ottobrunn, Germany, 7–11 September and the dynamic interactions between these subsystems will be presented while considering a selected generic hypersonic configuration. This vehicle configuration, similar to the X vehicle, is shown to be an unstable.

With the capability of high speed flying, a more reliable and cost efficient way to access space is provided by hypersonic flight vehicles. Controller design, as key technology to make hypersonic flight feasible and efficient, has numerous challenges stemming from large flight envelope with extreme range of operation conditions, strong interactions between elastic airframe, the propulsion Cited by: Abstract.

This chapter demonstrates the method to synthesize and simulate an H ∞ linear parameter-varying (LPV) controller for a flexible air-breathing hypersonic vehicle (HSV) model. The output feedback design used velocity tracking for both the flexible and rigid body hypersonic vehicle by: 2.

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of the 6th SIAM Conference on Parallel Processing for Scientific Computing,; Hendrickson and Leland Cited by: This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration l power demands are harmonized with static- dynamic- and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account.

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OPTIMAL CONTROL AND ESTIMATION, Dover Publications, New York, (originally published as STOCHASTIC OPTIMAL CONTROL; Theory and Application, J. Wiley & Sons, New York, ) In-Flight Simulation with Pilot-Center of Gravity Offset and Velocity Mismatch(pdf), Book Review: Morphing Aerospace Vehicles and Structures, J.

Valasek, ed. Publication List If you are "Fault and mode switching identification for hybrid systems with application to electro-hydraulic system in vehicles", Book Chapter (invited), {\it Intelligent Unmanned Systems: Theory and Applications.

Ronghu, "Neural Network based Terminal Iterative Learning Control for Uncertain Non-linear Non-a ne Systems. We investigate the adaptive tracking problem for the longitudinal dynamics of state-constrained airbreathing hypersonic vehicles, where not only the velocity and the altitude, but also the angle of attack (AOA) is required to be tracked.

A novel indirect AOA tracking strategy is proposed by viewing the pitch angle as a new output and devising Cited by: 2.Aerothermoelastic Modeling of Hypersonic Vehicles for Control Design Hypersonic Vehicle (HSV) Air-breathing hypersonic vehicles (HSV) present strong interactions among aerodynamics, elastic airframe and control effector deformations, heat transfer and propulsion system (itself .A new adaptive robust nonlinear predictive control law is designed in this paper to mitigate the damage during airfoil flutter of a generic hypersonic flight vehicle.

A three-degrees-of-freedom airfoil dynamic motion model is established, in which the third piston theory is Author: Xiaohui Zhang, Yuhui Wang, Xingkai Feng, Siyuan Hou.