3 edition of Real-time simulation model of the HL-20 lifting body found in the catalog.
Real-time simulation model of the HL-20 lifting body
by National Aeronautics and Space Administration, Langley Research Center, For sale by the National Technical Information Service in [Hampton, Va, Springfield, Va
Written in English
|Other titles||Real time simulation model of ....|
|Statement||E. Bruce Jackson, Christopher I. Cruz, W.A. Ragsdale.|
|Series||TM -- 107580., NASA technical memorandum -- 107580.|
|Contributions||Cruz, Christopher I., Ragsdale, W. A., Langley Research Center.|
|The Physical Object|
Arnold explained to io9 that this video has a frame rate of about 15 fps, so you are seeing the process about times that of real-time. More at io9, and read the scientific journal article in. The new design comprises other improvements of the HL that were developed before as part of the Orbital Space Plane (OSP) program by the NASA. The main di- fference is that the original HL has a pure lifting body, while the upgrade has a Blended Lifting Body (BLB).
This book is a selection of papers presented at the conference. All submitted papers have gone through a formal review process in compliance with good journal practices. The best papers have been recommended by the reviewers to be published in this book. Pressure: 7 PSI ( bar); Optional: PSI (10 bar) Extension ( mm) with Boot-Shaped Vane 1A _ _ Minimum Material Density: Standard Vane: Down to g/l; Hinged Vane: Length ( mm) with Boot-Shaped Vane 2A _ _ Wireless Sensing and Down to 15 g/l; (depends on shaft/vane coverage) Agency CSA/FM Dust Ignition Proof.
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Dynamic model of an early slab-wing version of the HL vehicle with a maximum lift-to-drag ratio of The model was developed to provide an early real-time simulation of the vehicle in the approach and landing phases of flight.
The simulation was used from February to October of to support devel-File Size: 2MB. This report documents the current real-time simulation model of the HL lifting body vehicle, known as versionpresently in use at NASA Langley Research Center.
Get this from a library. Real-time simulation model of the HL lifting body. [E Bruce Jackson; Christopher I Cruz; W A Ragsdale; Langley Research Center.]. HL Lifting Body, guidance and control law and simulation team leader Selected Publications (in reverse chronological order) Jackson, E.
B, Hoffler, K. D.: “Effects of Atmospheric Motion on a Derived Angle-of-Attack Estimator.”. Bruce Jackson. Adaptive Aerospace Group, Inc.
Preliminary subsonic aerodynamic model for simulation studies of the hl lifting body. NASA-TM, L. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Jackson, E.B., Cruz, C.I.: Preliminary Subsonic Aerodynamic Model for Simulation Studies of the HL Lifting Body.
NASA Technical Memorandum () Google Scholar by: 2. Aerospace and defense companies worldwide rely on MATLAB ® and Simulink ® across all technology readiness levels, from prototypes to their most important safety and mission critical and Simulink are used in major programs across all domains, such as the F Joint Strike Fighter and Mars Exploration Rover, and accelerate research and development in.
Aerospace Blockset™ provides Simulink ® blocks for modeling, simulating, and analyzing aerospace vehicles. You can incorporate vehicle dynamics, validated models of the flight environment, and pilot behavior, and then connect your model to the FlightGear Flight Simulator to visualize simulation results.
AIAA It can take weeks or months to incorporate a new aerodynamic model into a vehicle simulation and validate the performance of the : Engineer at Adaptive Aerospace.
The HL Crew Rescue Vehicle was based on the Personnel Launch System (PLS) concept being developed by NASA as an outgrowth of earlier lifting body research.
In OctoberRockwell International (Space Systems Division) began a year-long contracted effort managed by Langley Research Center to perform an in-depth study of PLS design and. Table 5 lists the mass properties used in the FASER simulation. Table 5. Mass Properties of the Simulated FASER Parameter Weight (lb) Ix (slug-ft') Iy (slug-ft") (slug-ft") Ixz (slug-ft") Value HL SIMULATION The NASA HL.
Assessment of an Inviscid Euler-Adjoint Solver for Prediction of Aerodynamic Characteristics of the NASA HL Lifting Body. Dan Almosnino; AIAA Real-Time Adaptive Least-Squares Drag Minimization for Performance Adaptive Aeroelastic Wing.
Model Reduction in Discrete Vortex Methods for 2D Unsteady Aerodynamic Flows. Posted 2/25/10 PM, messages. The DreamCha 88 is a reusable crewed spacecraft concept based on the NASA HL lifting body concept launched atop an Atlas V Evolved Expendable Launch Vehicle.
It is supported by a $20 million NASA CCDev contract. Full text of "Florian Holzapfel, Stephan Theil - Advances in Aerospace Guidance, Navigation and Control" See other formats. The lifting-body model reached the ground much sooner than did the tow-plane because the lifting body's much lower lift-to-drag ratio gave it a much steeper gliding angle.
The M2-F1 made a good landing on Sterks' dirt strip, while the tow-plane landed unharmed in 5/5(1). HL Lifting Body Added: Aug | Visits: This model uses Simulink and the Aerospace Blockset for modeling the airframe of a NASA HL lifting body, which is a low-cost complement to the Space Shuttle orbiter.
prototype real-time guidance and targeting algorithms. , NASA’s HL , and the Sierra Nevada Corporation’s Dream Chaser . Figure 5 shows an example bank-angle steering maneuver for a blunt body vehicle: However, winged and lifting body vehi-cles that possess aerodynamic control surfaces capable of countering the.
the 23rd european modeling & simulation symposium september rome, italy edited by agostino g. bruzzone miquel a. piera francesco longo priscilla elfrey michael affenzeller osman balci printed in rende (cs), italy, september isbn i.
- Cópia - Free download as PDF File .pdf), Text File .txt) or read online for free. A Collection of Nonlinear Aircraft Simulations in MATLAB.This report documents the current real-time simulation model of the HL lifting body vehicle, known as versionpresently in use at NASA Langley Research Center.
Included are data on vehicle aerodynamics, inertias, geometries, guidance and control laws, and .E. Bruce Jackson and Christopher I. Cruz, Preliminary Subsonic Aerodynamic Model for Simulation Studies of the HL Lifting Body, NASA TM, Augustpp.
Richard S. Pappa, Axel Schenk and Christopher Noll, Eigensystem Realization Algorithm Modal Identification Experiences With Mini-Mast, NASA TM, Februarypp.