Thrust Vectoring on the NASA F-18 High Alpha Research Vehicle
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[1] J. R. Chambers. High-angle-of-attack aerodynamics - Lessons learned , 1986 .
[2] Steven A. Johnson. Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes , 1992 .
[3] Francis J. Capone,et al. Multiaxis aircraft control power from thrust vectoring at high angles of attack , 1986 .
[4] R. E. Maine,et al. Application of parameter estimation to aircraft stability and control: The output-error approach , 1986 .
[5] Marcello R. Napolitano,et al. Parameter estimation for the NASA F/A-18 HARV at high angles of attack , 1994 .
[6] Marcello R. Napolitano,et al. Estimation of the lateral-directional aerodynamic parameters from flight data for the NASA F/A-18 HARV , 1996 .
[7] Joseph W. Pahle,et al. Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle , 1996 .
[8] M. L. Mason,et al. Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles , 1985 .
[9] James E. Murray,et al. The pEst version 2.1 user's manual , 1987 .
[10] Mary L. Mason,et al. Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes , 1988 .
[11] R. E. Maine,et al. Identification of dynamic systems, theory and formulation , 1985 .
[12] F. J. Capone,et al. Investigation of axisymmetric and nonaxisymmetric nozzles installed on a 0.10 scale F-18 prototype airplane model. [wind tunnel tests] , 1980 .
[13] C Asbury Scott,et al. Multiaxis Thrust-Vectoring Characteristics of a Model Representative of the F-18 High-Alpha Research Vehicle at Angles of Attack From 0 to 70 , 1995 .
[14] D. Antani,et al. Static test results of an externally mounted thrust vectoring vane concept , 1988 .
[15] Ronald J. Ray. Evaluation of various thrust calculation techniques on an F404 engine , 1990 .
[16] B. L. Berrier,et al. Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60 deg , 1984 .
[17] Victoria Regenie,et al. The F-18 High Alpha Research Vehicle: A High-Angle-of-Attack Testbed Aircraft , 1992 .
[18] Joseph W. Pahle,et al. Research flight-control system development for the F-18 high alpha research vehicle , 1991 .
[19] Albion H. Bowers,et al. F-18 high alpha research vehicle: Lessons learned , 1994 .
[20] Eugene A. Morelli. Flight Test Validation of Optimal Input Design Using Pilot Implementation , 1994 .
[21] Brad Seanor,et al. Estimation of the longitudinal aerodynamic parameters from flight data for the NASA F/A-18 HARV , 1996 .
[22] Russell J. Gates,et al. A comparison of flight input techniques for parameter estimation of highly-augmented aircraft , 1996 .
[23] M. L. Mason,et al. Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring , 1988 .
[24] C Asbury Scott,et al. A Static Investigation of the Thrust Vectoring System of the F/A-18 High-Alpha Research Vehicle , 1992 .
[25] M. L. Mason,et al. Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle , 1991 .