Stability Derivative Extraction from Flight Test Data for a General Aviation Aircraft

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ISBN 13 :
Total Pages : 236 pages
Book Rating : 4.:/5 (377 download)

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Book Synopsis Stability Derivative Extraction from Flight Test Data for a General Aviation Aircraft by : Brian Edward Randall

Download or read book Stability Derivative Extraction from Flight Test Data for a General Aviation Aircraft written by Brian Edward Randall and published by . This book was released on 1996 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Real-Time Stability and Control Derivative Extraction From F-15 Flight Data

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Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Real-Time Stability and Control Derivative Extraction From F-15 Flight Data by : Mark S. Smith

Download or read book Real-Time Stability and Control Derivative Extraction From F-15 Flight Data written by Mark S. Smith and published by . This book was released on 2003 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation by : George G. Steinmetz

Download or read book Longitudinal Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation written by George G. Steinmetz and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A method of parameter extraction for stability and control derivatives of aircraft from flight test data, implementing maximum likelihood estimation, has been developed and successfully applied to actual longitudinal flight test data from a modern sophisticated jet fighter. The results of this application establish the merits of the estimation technique and its computer implementation (allowing full analyst interaction with the program) as well as provide data for the validation of a portion of the Langley differential maneuvering simulator (DMS). The results are presented for all flight test runs in tabular form and as time history comparisons between the estimated states and the actual flight test data."--Page i

Final Report on Extraction of Aircraft Stability Coefficients from Flight Test Data and Theoretical and Experimental Studies on Selected Problems of High Speed Aerodynamics and Dynamic Stability

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ISBN 13 :
Total Pages : 154 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Final Report on Extraction of Aircraft Stability Coefficients from Flight Test Data and Theoretical and Experimental Studies on Selected Problems of High Speed Aerodynamics and Dynamic Stability by : Lloyd Eugene Wilkie

Download or read book Final Report on Extraction of Aircraft Stability Coefficients from Flight Test Data and Theoretical and Experimental Studies on Selected Problems of High Speed Aerodynamics and Dynamic Stability written by Lloyd Eugene Wilkie and published by . This book was released on 1957 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Determination of Stability and Control Parameters of a General Aviation Airplane from Flight Data

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Determination of Stability and Control Parameters of a General Aviation Airplane from Flight Data by : Imran Abbasy

Download or read book Determination of Stability and Control Parameters of a General Aviation Airplane from Flight Data written by Imran Abbasy and published by . This book was released on 1983 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Lateral Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation

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Publisher :
ISBN 13 :
Total Pages : 51 pages
Book Rating : 4.:/5 (223 download)

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Book Synopsis Lateral Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation by : Russell V. Parrish

Download or read book Lateral Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation written by Russell V. Parrish and published by . This book was released on 1972 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method of parameter extraction for stability and control derivatives of aircraft from flight test data, implementing maximum likelihood estimation, has been developed and successfully applied to actual lateral flight test data from a modern sophisticated jet fighter. This application demonstrates the important role played by the analyst in combining engineering judgment and estimator statistics to yield meaningful results. During the analysis, the problems of uniqueness of the extracted set of parameters and of longitudinal coupling effects were encountered and resolved. The results for all flight runs are presented in tabular form and as time history comparisons between the estimated states and the actual flight test data.

Real-Time Stability and Control Derivative Extraction from F-15 Flight Data

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Publisher : Independently Published
ISBN 13 : 9781723750137
Total Pages : 38 pages
Book Rating : 4.7/5 (51 download)

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Book Synopsis Real-Time Stability and Control Derivative Extraction from F-15 Flight Data by : National Aeronautics and Space Adm Nasa

Download or read book Real-Time Stability and Control Derivative Extraction from F-15 Flight Data written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-16 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A real-time, frequency-domain, equation-error parameter identification (PID) technique was used to estimate stability and control derivatives from flight data. This technique is being studied to support adaptive control system concepts currently being developed by NASA (National Aeronautics and Space Administration), academia, and industry. This report describes the basic real-time algorithm used for this study and implementation issues for onboard usage as part of an indirect-adaptive control system. A confidence measures system for automated evaluation of PID results is discussed. Results calculated using flight data from a modified F-15 aircraft are presented. Test maneuvers included pilot input doublets and automated inputs at several flight conditions. Estimated derivatives are compared to aerodynamic model predictions. Data indicate that the real-time PID used for this study performs well enough to be used for onboard parameter estimation. For suitable test inputs, the parameter estimates converged rapidly to sufficient levels of accuracy. The devised confidence measures used were moderately successful.Smith, Mark S. and Moes, Timothy R. and Morelli, Eugene A.Armstrong Flight Research Center; Langley Research CenterF-15 AIRCRAFT; PARAMETER IDENTIFICATION; REAL TIME OPERATION; STABILITY DERIVATIVES; CONTROL STABILITY; CONTROL SYSTEMS DESIGN; FREQUENCY DOMAIN ANALYSIS; FLIGHT CONDITIONS; INDUSTRIES; NASA PROGRAMS; FOURIER TRANSFORMATION; REGRESSION ANALYSIS; ALGORITHMS; ERROR ANALYSIS; ONBOARD DATA PROCESSING

Lateral Stability and Control Derivates of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation

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Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Lateral Stability and Control Derivates of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation by : Russell V. Parrish

Download or read book Lateral Stability and Control Derivates of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation written by Russell V. Parrish and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Determination of Aircraft Stability Coefficients from Flight Test Data

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Publisher :
ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Determination of Aircraft Stability Coefficients from Flight Test Data by : Lloyd Eugene Wilkie

Download or read book The Determination of Aircraft Stability Coefficients from Flight Test Data written by Lloyd Eugene Wilkie and published by . This book was released on 1958 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Flight Test System for the Determination of the Stability and Control Derivatives of a General Aviation Aircraft

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Publisher :
ISBN 13 :
Total Pages : 288 pages
Book Rating : 4.:/5 (351 download)

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Book Synopsis A Flight Test System for the Determination of the Stability and Control Derivatives of a General Aviation Aircraft by : David Christopher Oehl

Download or read book A Flight Test System for the Determination of the Stability and Control Derivatives of a General Aviation Aircraft written by David Christopher Oehl and published by . This book was released on 1995 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane

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ISBN 13 :
Total Pages : 204 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane by : Ernest L. Black

Download or read book Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane written by Ernest L. Black and published by . This book was released on 1969 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Determination of Aircraft Stability Coefficients from Flight-test Data

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ISBN 13 :
Total Pages : 152 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Determination of Aircraft Stability Coefficients from Flight-test Data by : Lloyd Eugene Wilkie

Download or read book The Determination of Aircraft Stability Coefficients from Flight-test Data written by Lloyd Eugene Wilkie and published by . This book was released on 1958 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Lateral Stability and Control Derivatives of a Jet Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation

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ISBN 13 :
Total Pages : 51 pages
Book Rating : 4.:/5 (113 download)

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Book Synopsis Lateral Stability and Control Derivatives of a Jet Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation by : Russell V. Parrish

Download or read book Lateral Stability and Control Derivatives of a Jet Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation written by Russell V. Parrish and published by . This book was released on 1972 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Stability and Automatic Control

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Publisher : WCB/McGraw-Hill
ISBN 13 : 9780071158381
Total Pages : 441 pages
Book Rating : 4.1/5 (583 download)

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Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.

Comparison of Several Methods for Estimating Low-speed Stability Derivatives for Two Airplane Configurations

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Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Comparison of Several Methods for Estimating Low-speed Stability Derivatives for Two Airplane Configurations by : Herman S. Fletcher

Download or read book Comparison of Several Methods for Estimating Low-speed Stability Derivatives for Two Airplane Configurations written by Herman S. Fletcher and published by . This book was released on 1971 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods presented in five different publications have been used to estimate the low-speed stability derivatives of two unpowered airplane configurations. One configuration had unswept lifting surfaces, the other configuration was the D-558-II swept-wing research airplane. The results of the computations were compared with each other, with existing wind-tunnel data, and with flight-test data for the D-558-II configuration to assess the relative merits of the methods for estimating derivatives. The results of the study indicated that, in general, for low subsonic speeds, no one text appeared consistently better for estimating all derivatives.

A Comparison and Evaluation of Two Methods of Extracting Stability Derivatives from Flight Test Data

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ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis A Comparison and Evaluation of Two Methods of Extracting Stability Derivatives from Flight Test Data by : Paul W. Kirster

Download or read book A Comparison and Evaluation of Two Methods of Extracting Stability Derivatives from Flight Test Data written by Paul W. Kirster and published by . This book was released on 1974 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two methods for extracting stability derivatives from flight data are compared. A modified Newton-Raphson minimization technique and a digital-analog (hybrid) matching technique were used to analyze the same data maneuvers obtained from two aircraft. About 55 maneuvers of an F-111E aircraft were analyzed over a Mach number range of 0.3 to 2.0 and an angle of attack range of 3 to 19 degrees. About 15 maneuvers were analyzed for the X-24A lifting body at Mach numbers of 0.8 and 0.9 and an angle of attack range of 4 to 13 degrees. Stability derivatives were extracted from these maneuvers, and the results from the two techniques along with wind tunnel results were compared. (Modified author abstract).

Flight Testing Techniques for the Evaluation of Light Aircraft Stability Derivatives: A Review and Analysis

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Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flight Testing Techniques for the Evaluation of Light Aircraft Stability Derivatives: A Review and Analysis by : Frederick O. Smetana

Download or read book Flight Testing Techniques for the Evaluation of Light Aircraft Stability Derivatives: A Review and Analysis written by Frederick O. Smetana and published by . This book was released on 1972 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: