-
1
-
-
84888974614
-
Flight measurements of stability and control derivatives of the X-15 research airplane to a mach number of 6.02 and an angle of attack of 25 deg
-
Nov.
-
Yancey, R. B., "Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25 Deg," NASA-TN-D-2532, Nov. 1964.
-
(1964)
NASA-TN-D-2532
-
-
Yancey, R.B.1
-
2
-
-
84888964186
-
Evaluation of the lateral-directional stability and control characteristics of the lightweight M2-F1 lifting body at low speeds
-
Sept.
-
Smith, H. J., "Evaluation of the Lateral-Directional Stability and Control Characteristics of the Lightweight M2-F1 Lifting Body at Low Speeds," NASA TN-D-3022, Sept. 1965.
-
(1965)
NASA TN-D-3022
-
-
Smith, H.J.1
-
4
-
-
84888936463
-
-
Air Force Flight Test Center, FTC-TDR-64-8, Edwards AFB, CA, May
-
Rampy, J. M., and Barry, D. T., "Determination of Stability Derivatives from Flight Test Data by Means of High Speed Repetitive Operation Analog Matching," Air Force Flight Test Center, FTC-TDR-64-8, Edwards AFB, CA, May 1964.
-
(1964)
Determination of Stability Derivatives from Flight Test Data by Means of High Speed Repetitive Operation Analog Matching
-
-
Rampy, J.M.1
Barry, D.T.2
-
5
-
-
84888952354
-
The determination of lateral stability and control derivatives from flight data
-
Howard, J., "The Determination of Lateral Stability and Control Derivatives from Flight Data," Canadian Aeronautics Space Journal, Vol. 13, No. 3, 1967, pp. 126-134.
-
(1967)
Canadian Aeronautics Space Journal
, vol.13
, Issue.3
, pp. 126-134
-
-
Howard, J.1
-
6
-
-
79951650974
-
On the analysis of linear and non-linear dynamical systems from transient response data
-
Dec.
-
Shinbrot, M., "On the Analysis of Linear and Non-Linear Dynamical Systems from Transient Response Data," NACA TN-3288, Dec. 1954.
-
(1954)
NACA TN-3288
-
-
Shinbrot, M.1
-
7
-
-
3743144607
-
A survey of methods for determining stability parameters of an airplane from dynamic flight measurement
-
April
-
Greenberg, H., "A Survey of Methods for Determining Stability Parameters of an Airplane From Dynamic Flight Measurement," NACA TN-2340, April 1951.
-
(1951)
NACA TN-2340
-
-
Greenberg, H.1
-
8
-
-
84888974882
-
Summary of dynamic stability and control flight research conducted utilizing a B-25J airplane
-
Buffalo, New York, May
-
Breuhaus, W. O., "Summary of Dynamic Stability and Control Flight Research Conducted Utilizing a B-25J Airplane," Cornell Aeronautical Lab., Rept. TB-405-F-10, Buffalo, New York, May 1948.
-
(1948)
Cornell Aeronautical Lab., Rept.
, vol.TB-405-F-10
-
-
Breuhaus, W.O.1
-
9
-
-
3743080167
-
The pulse method for the determination of aircraft dynamic performance
-
Seamans, R. C., Jr., Blasingame, B. P., and Clementson, G. C., "The Pulse Method for the Determination of Aircraft Dynamic Performance," Journal of the Aeronautical Sciences, Vol. 17, No. 1, 1950, pp. 22-38.
-
(1950)
Journal of the Aeronautical Sciences
, vol.17
, Issue.1
, pp. 22-38
-
-
Seamans Jr., R.C.1
Blasingame, B.P.2
Clementson, G.C.3
-
10
-
-
3743054407
-
Application of advanced identification techniques to nonlinear equations of motion
-
Wright-Patterson Air Force Base, Ohio, Dec.
-
Rynaski, E. G., "Application of Advanced Identification Techniques to Nonlinear Equations of Motion," Proceedings of the Stall/Post-Stall/Spin Symposium, Wright-Patterson Air Force Base, Ohio, Dec. 1971, pp. 0-1-0-18.
-
(1971)
Proceedings of the Stall/Post-stall/Spin Symposium
, pp. 1-18
-
-
Rynaski, E.G.1
-
11
-
-
0346571273
-
Determination of stability derivatives from flight data using a Newton-Raphson minimization technique
-
Iliff, K. W., and Taylor, L. W., Jr., "Determination of Stability Derivatives from Flight Data Using a Newton-Raphson Minimization Technique," NASA TN D-6579, 1972.
-
(1972)
NASA TN D-6579
-
-
Iliff, K.W.1
Taylor Jr., L.W.2
-
13
-
-
0039995806
-
Stochastic system identification techniques
-
edited by H. F. Karreman, Wiley, London
-
Balakrishnan, A. V., "Stochastic System Identification Techniques," Stochastic Optimization and Control, edited by H. F. Karreman, Wiley, London, 1968.
-
(1968)
Stochastic Optimization and Control
-
-
Balakrishnan, A.V.1
-
14
-
-
3743111281
-
A modified Newton-Raphson method for determining stability derivatives from flight data
-
Academic Press, New York
-
Taylor, L. W., Jr., and Iliff, K. W., "A Modified Newton-Raphson Method for Determining Stability Derivatives from Flight Data," Second International Conference on Computing Methods in Optimization Problems, Academic Press, New York, 1969, pp. 353-364.
-
(1969)
Second International Conference on Computing Methods in Optimization Problems
, pp. 353-364
-
-
Taylor Jr., L.W.1
Iliff, K.W.2
-
15
-
-
44649104366
-
A comparison of Newton-Raphson and other methods for determining stability derivatives from flight data
-
NASA Ames Research Center, Moffett Field, CA, Nov.
-
Taylor, L. W., Jr., Iliff, K. W., and Powers, B. G., "A Comparison of Newton-Raphson and Other Methods for Determining Stability Derivatives from Flight Data," Third Technical Workshop on Dynamic Stability Problems, NASA Ames Research Center, Moffett Field, CA, Nov. 1968.
-
(1968)
Third Technical Workshop on Dynamic Stability Problems
-
-
Taylor Jr., L.W.1
Iliff, K.W.2
Powers, B.G.3
-
16
-
-
84888960843
-
A comparison of Newton-Raphson and other methods for determining stability derivatives from flight data
-
March
-
Iliff, K. W., Powers, B. G., and Taylor, L. W., Jr., "A Comparison of Newton-Raphson and Other Methods for Determining Stability Derivatives from Flight Data," AIAA Paper 69-315, March 1969.
-
(1969)
AIAA Paper
, vol.69
, Issue.315
-
-
Iliff, K.W.1
Powers, B.G.2
Taylor Jr., L.W.3
-
17
-
-
4344647514
-
The measurement of the damping in roll on a JN4h in flight
-
Norton, F. H., "The Measurement of the Damping in Roll on a JN4h in Flight," NACA Rept. 167, 1923.
-
(1923)
NACA Rept.
, vol.167
-
-
Norton, F.H.1
-
18
-
-
3743088979
-
A study of longitudinal dynamic stability in flight
-
Norton, F. H., "A Study of Longitudinal Dynamic Stability in Flight," NACA Rept. 170, 1923.
-
(1923)
NACA Rept.
, vol.170
-
-
Norton, F.H.1
-
19
-
-
17044428987
-
Stochastic differential system I
-
edited by M. Beckman, G. Goos, and H. P. Kunzi, Lecture Notes in Economics and Mathematical Systems, Springer-Verlag, Berlin
-
Balakrishnan, A. V., "Stochastic Differential System I," Filtering and Control; A Function Space Approach, edited by M. Beckman, G. Goos, and H. P. Kunzi, Lecture Notes in Economics and Mathematical Systems, Vol. 84, Springer-Verlag, Berlin, 1973.
-
(1973)
Filtering and Control; A Function Space Approach
, vol.84
-
-
Balakrishnan, A.V.1
-
20
-
-
84888947434
-
Maximum likelihood estimates of lift and drag characteristics obtained from dynamic aircraft maneuvers
-
AIAA, New York
-
Iliff, K. W., "Maximum Likelihood Estimates of Lift and Drag Characteristics Obtained from Dynamic Aircraft Maneuvers," Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference, AIAA, New York, 1976, pp. 137-150; also Journal of Aircraft, Vol. 14, No. 12, 1977, pp. 1175-1181.
-
(1976)
Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference
, pp. 137-150
-
-
Iliff, K.W.1
-
21
-
-
0017630710
-
-
Iliff, K. W., "Maximum Likelihood Estimates of Lift and Drag Characteristics Obtained from Dynamic Aircraft Maneuvers," Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference, AIAA, New York, 1976, pp. 137-150; also Journal of Aircraft, Vol. 14, No. 12, 1977, pp. 1175-1181.
-
(1977)
Journal of Aircraft
, vol.14
, Issue.12
, pp. 1175-1181
-
-
-
22
-
-
85003251847
-
Flight test results of an active flutter suppression system installed on a remotely piloted research vehicle
-
Edwards, J. W., "Flight Test Results of an Active Flutter Suppression System Installed on a Remotely Piloted Research Vehicle," NASA TM-83132, 1981.
-
(1981)
NASA TM-83132
-
-
Edwards, J.W.1
-
23
-
-
4344713196
-
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
-
Dec.
-
Iliff, K. W., and Wang, K. C., "Flight-Determined Subsonic Longitudinal Stability and Control Derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with Thrust Vectoring," NASA TP-97-206539, Dec. 1997.
-
(1997)
NASA TP-97-206539
-
-
Iliff, K.W.1
Wang, K.C.2
-
24
-
-
0005890756
-
Flight-determined subsonic lateral-directional stability and control derivatives of the thrust-vectoring F-18 High Angle of Attack Research Vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives
-
Jan.
-
Iliff, K. W., and Wang, K. C., "Flight-Determined Subsonic Lateral-Directional Stability and Control Derivatives of the Thrust-Vectoring F-18 High Angle of Attack Research Vehicle (HARV), and Comparisons to the Basic F-18 and Predicted Derivatives," NASA TP-99-206573, Jan. 1999.
-
(1999)
NASA TP-99-206573
-
-
Iliff, K.W.1
Wang, K.C.2
-
25
-
-
0040547606
-
Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8-scale F-15 airplane model obtained from flight test
-
Jan.
-
Iliff, K. W., Maine, R. E., and Shafer, M. F., "Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8-Scale F-15 Airplane Model Obtained From Flight Test," NASA TN-D-8136, Jan. 1976.
-
(1976)
NASA TN-D-8136
-
-
Iliff, K.W.1
Maine, R.E.2
Shafer, M.F.3
-
26
-
-
3743076830
-
-
Ph.D. Dissertation, UCLA-ENG-7430, Univ. of California, Los Angeles, May
-
Iliff, K. W., "Identification and Stochastic Control with Application to Flight Control in Turbulence," Ph.D. Dissertation, UCLA-ENG-7430, Univ. of California, Los Angeles, May 1973.
-
(1973)
Identification and Stochastic Control with Application to Flight Control in Turbulence
-
-
Iliff, K.W.1
-
27
-
-
4344675478
-
Estimation of characteristics and stochastic control of an aircraft flying in atmospheric turbulence
-
AIAA, New York
-
Iliff, K. W., "Estimation of Characteristics and Stochastic Control of an Aircraft Flying in Atmospheric Turbulence," Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference, AIAA, New York, 1976, pp. 26-38; also Journal of Guidance and Control, Vol. 1, No.2, 1978, pp. 101-108.
-
(1976)
Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference
, pp. 26-38
-
-
Iliff, K.W.1
-
28
-
-
85003360405
-
-
Iliff, K. W., "Estimation of Characteristics and Stochastic Control of an Aircraft Flying in Atmospheric Turbulence," Proceedings of the AIAA 3rd Atmospheric Flight Mechanics Conference, AIAA, New York, 1976, pp. 26-38; also Journal of Guidance and Control, Vol. 1, No.2, 1978, pp. 101-108.
-
(1978)
Journal of Guidance and Control
, vol.1
, Issue.2
, pp. 101-108
-
-
-
29
-
-
0041183064
-
User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
-
Nov.
-
Maine, R. E., and Iliff, K. W., "User's Manual for MMLE3, A General FORTRAN Program for Maximum Likelihood Parameter Estimation," NASA TP-1563, Nov. 1980.
-
(1980)
NASA TP-1563
-
-
Maine, R.E.1
Iliff, K.W.2
-
30
-
-
0040588978
-
Programmer's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
-
June
-
Maine, R. E., "Programmer's Manual for MMLE3, A General FORTRAN Program for Maximum Likelihood Parameter Estimation," NASA TP-1690, June 1981.
-
(1981)
NASA TP-1690
-
-
Maine, R.E.1
-
31
-
-
0020912357
-
Minimum testing of the space shuttle orbiter for stability and control derivatives
-
edited by J. P. Arrington and J. J. Jones, NASA Langley Research Center, NASA CP-2283, Hampton, VA
-
Cooke, D. R., "Minimum Testing of the Space Shuttle Orbiter for Stability and Control Derivatives," Shuttle Performance: Lessons Learned, edited by J. P. Arrington and J. J. Jones, NASA Langley Research Center, NASA CP-2283, Hampton, VA, Pt. 1, 1983, pp. 447-471.
-
(1983)
Shuttle Performance: Lessons Learned
, Issue.PART 1
, pp. 447-471
-
-
Cooke, D.R.1
-
32
-
-
0020892652
-
Predicted and flight test results of the performance, stability and control of the space shuttle from reentry to landing
-
edited by J. P. Arrington and J. J. Jones, NASA Langley Research Center, NASA CP-2283, Hampton, VA
-
Kirsten, P. W., Richardson, D. F., and Wilson, C. M., "Predicted and Flight Test Results of the Performance, Stability and Control of the Space Shuttle From Reentry to Landing," Shuttle Performance: Lessons Learned, edited by J. P. Arrington and J. J. Jones, NASA Langley Research Center, NASA CP-2283, Hampton, VA, Pt. 1, 1983, pp. 509-524.
-
(1983)
Shuttle Performance: Lessons Learned
, Issue.PART 1
, pp. 509-524
-
-
Kirsten, P.W.1
Richardson, D.F.2
Wilson, C.M.3
-
33
-
-
84888963323
-
Extraction of stability and control derivatives from orbiter flight data
-
June
-
Iliff, K. W., and Shafer, M. F., "Extraction of Stability and Control Derivatives from Orbiter Flight Data," NASA TM-4500, June 1993.
-
(1993)
NASA TM-4500
-
-
Iliff, K.W.1
Shafer, M.F.2
-
34
-
-
11544365177
-
The pEst version 2.1 user's manual
-
Sept.
-
Murray, J. E., and Maine, R. E., "The pEst Version 2.1 User's Manual," NASA TM-88280, Sept. 1987.
-
(1987)
NASA TM-88280
-
-
Murray, J.E.1
Maine, R.E.2
-
35
-
-
0029696291
-
Evolution of flight vehicle system identification
-
Hamel, P. G., and Jategaonkar, R. V., "Evolution of Flight Vehicle System Identification," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 9-28.
-
(1996)
Journal of Aircraft
, vol.33
, Issue.1
, pp. 9-28
-
-
Hamel, P.G.1
Jategaonkar, R.V.2
-
36
-
-
0030144414
-
X-31A system identification using single-surface excitation at high angles of attack
-
Weiss, S., Friehmelt, F. H., Plaetschke, E., and Rohlf, D., "X-31A System Identification Using Single-Surface Excitation at High Angles of Attack," Journal of Aircraft, Vol. 33, No. 3, 1996, pp. 485-490.
-
(1996)
Journal of Aircraft
, vol.33
, Issue.3
, pp. 485-490
-
-
Weiss, S.1
Friehmelt, F.H.2
Plaetschke, E.3
Rohlf, D.4
-
37
-
-
0004865510
-
Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain
-
Klein, V., "Maximum Likelihood Method for Estimating Airplane Stability and Control Parameters From Flight Data in Frequency Domain," NASA TP-1637, 1980.
-
(1980)
NASA TP-1637
-
-
Klein, V.1
-
38
-
-
0344865116
-
Practical input optimization for aircraft parameter estimation experiments
-
May
-
Morelli, E. A., "Practical Input Optimization for Aircraft Parameter Estimation Experiments," NASA CR-191242, May 1993.
-
(1993)
NASA CR-191242
-
-
Morelli, E.A.1
-
39
-
-
85039489118
-
On the adequate model for aircraft parameter estimation
-
England, U.K., March
-
Klein, V., "On the Adequate Model for Aircraft Parameter Estimation," Cranfield Inst. of Technology, Cranfield Rept. Aero No. 28, England, U.K., March 1975.
-
(1975)
Cranfield Inst. of Technology, Cranfield Rept. Aero No. 28
, vol.28
-
-
Klein, V.1
-
40
-
-
0004266961
-
System identification methods for aircraft flight control development and validation
-
Oct.
-
Tischler, M. B., "System Identification Methods for Aircraft Flight Control Development and Validation," NASA TM-110369, Oct. 1995.
-
(1995)
NASA TM-110369
-
-
Tischler, M.B.1
-
41
-
-
85040272091
-
The theory and practice of estimating the accuracy of dynamic flight-determined coefficients
-
July
-
Maine, R. E., and Iliff, K. W., "The Theory and Practice of Estimating the Accuracy of Dynamic Flight-Determined Coefficients," NASA RP-1077, July 1981.
-
(1981)
NASA RP-1077
-
-
Maine, R.E.1
Iliff, K.W.2
-
42
-
-
0038027993
-
Identification of dynamic systems, theory and formulation
-
Feb.
-
Maine, R. E., and Iliff, K. W., "Identification of Dynamic Systems, Theory and Formulation," NASA RP-1138, Feb. 1985; also AGARD-AG-300, Vol. 2, 1985.
-
(1985)
NASA RP-1138
-
-
Maine, R.E.1
Iliff, K.W.2
-
43
-
-
85039501414
-
-
Maine, R. E., and Iliff, K. W., "Identification of Dynamic Systems, Theory and Formulation," NASA RP-1138, Feb. 1985; also AGARD-AG-300, Vol. 2, 1985.
-
(1985)
AGARD-AG-300
, vol.2
-
-
-
44
-
-
0022736591
-
Application of parameter estimation to aircraft stability and control: The output-error approach
-
June
-
Maine, R. E., and Iliff, K. W., "Application of Parameter Estimation to Aircraft Stability and Control: The Output-Error Approach," NASA RP-1168, June 1986.
-
(1986)
NASA RP-1168
-
-
Maine, R.E.1
Iliff, K.W.2
-
45
-
-
84888932709
-
Aircraft parameter estimation
-
Jan.
-
Iliff, K. W., "Aircraft Parameter Estimation," NASA TM-88281, Jan. 1987; also AIAA Paper CP-87-0623, Jan. 1987.
-
(1987)
NASA TM-88281
-
-
Iliff, K.W.1
-
46
-
-
84888946966
-
-
Jan.
-
Iliff, K. W., "Aircraft Parameter Estimation," NASA TM-88281, Jan. 1987; also AIAA Paper CP-87-0623, Jan. 1987.
-
(1987)
AIAA Paper
, vol.CP-87-0623
-
-
-
47
-
-
0019705986
-
Formulation and implementation of a practical algorithm for parameter estimation with process and measurement noise
-
Maine, R. E., and Iliff, K. W., "Formulation and Implementation of a Practical Algorithm for Parameter Estimation with Process and Measurement Noise," SIAM Journal of Applied Mathematics, Vol. 41, 1981, pp. 558-579.
-
(1981)
SIAM Journal of Applied Mathematics
, vol.41
, pp. 558-579
-
-
Maine, R.E.1
Iliff, K.W.2
-
48
-
-
0347201430
-
Practical aspects of using a maximum likelihood estimation method to extract stability and control derivatives from flight data
-
April
-
Iliff, K. W., and Maine, R. E., "Practical Aspects of Using a Maximum Likelihood Estimation Method to Extract Stability and Control Derivatives from Flight Data," NASA TN D-8209, April 1976.
-
(1976)
NASA TN D-8209
-
-
Iliff, K.W.1
Maine, R.E.2
-
49
-
-
85003411161
-
Important factors in the maximum likelihood analysis of flight test maneuvers
-
April
-
Iliff, K. W., Maine, R. E., and Montgomery, T. D., "Important Factors in the Maximum Likelihood Analysis of Flight Test Maneuvers," NASA TP-1459, April 1979.
-
(1979)
NASA TP-1459
-
-
Iliff, K.W.1
Maine, R.E.2
Montgomery, T.D.3
-
50
-
-
0004280732
-
-
AIAA CP-84-2070, Aug.
-
Iliff, K. W., and Maine, R. E., "More Than You May Want to Know About Maximum Likelihood Estimation," AIAA CP-84-2070, Aug. 1984; also NASA TM-85905, Jan. 1985.
-
(1984)
More than You May Want to Know about Maximum Likelihood Estimation
-
-
Iliff, K.W.1
Maine, R.E.2
-
51
-
-
84888968535
-
-
Jan.
-
Iliff, K. W., and Maine, R. E., "More Than You May Want to Know About Maximum Likelihood Estimation," AIAA CP-84-2070, Aug. 1984; also NASA TM-85905, Jan. 1985.
-
(1985)
NASA TM-85905
-
-
-
52
-
-
2742527203
-
Application of parameter estimation to highly unstable aircraft
-
Aug.
-
Maine, R. E., and Murray, J. E., "Application of Parameter Estimation to Highly Unstable Aircraft," NASA TM-88266, Aug. 1986.
-
(1986)
NASA TM-88266
-
-
Maine, R.E.1
Murray, J.E.2
-
53
-
-
0022791323
-
Bibliography for aircraft parameter estimation
-
Oct.
-
Iliff, K. W., and Maine, R. E., "Bibliography for Aircraft Parameter Estimation," NASA TM-86804, Oct. 1986.
-
(1986)
NASA TM-86804
-
-
Iliff, K.W.1
Maine, R.E.2
-
54
-
-
77950575774
-
X-29A lateral-directional stability and control derivatives from high-angle-of-attack flight data
-
Dec.
-
Iliff, K. W., and Wang, K. C., "X-29A Lateral-Directional Stability and Control Derivatives from High-Angle-of-Attack Flight Data," NASA TP-3664, Dec. 1996.
-
(1996)
NASA TP-3664
-
-
Iliff, K.W.1
Wang, K.C.2
-
55
-
-
0003901935
-
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
-
Feb.
-
Iliff, K. W., and Wang, K. C., "Extraction of Lateral-Directional Stability and Control Derivatives for the Basic F-18 Aircraft at High Angles of Attack," NASA TM-4786, Feb. 1997.
-
(1997)
NASA TM-4786
-
-
Iliff, K.W.1
Wang, K.C.2
-
56
-
-
84888951795
-
Stability and control estimation flight test results for the SR-71 aircraft with externally mounted experiments
-
June
-
Moes, T. R., and Iliff, K. W., "Stability and Control Estimation Flight Test Results for the SR-71 Aircraft With Externally Mounted Experiments," NASA TP-2002-210718, June 2002.
-
(2002)
NASA TP-2002-210718
-
-
Moes, T.R.1
Iliff, K.W.2
-
57
-
-
84888976229
-
Flight stability and control and performance results from the linear aerospike SR-71 experiment (LASRE)
-
Aug.
-
Moes, T. R., Cobleigh, B. R., Cox, T. H., Conners, T. R., Iliff, K. W., and Powers, B. G., "Flight Stability and Control and Performance Results from the Linear Aerospike SR-71 Experiment (LASRE)," NASA TM-1998-206565, Aug. 1998; also AIAA Paper CP-98-4340, Aug. 1998.
-
(1998)
NASA TM-1998-206565
-
-
Moes, T.R.1
Cobleigh, B.R.2
Cox, T.H.3
Conners, T.R.4
Iliff, K.W.5
Powers, B.G.6
-
58
-
-
84888942615
-
-
Aug.
-
Moes, T. R., Cobleigh, B. R., Cox, T. H., Conners, T. R., Iliff, K. W., and Powers, B. G., "Flight Stability and Control and Performance Results from the Linear Aerospike SR-71 Experiment (LASRE)," NASA TM-1998-206565, Aug. 1998; also AIAA Paper CP-98-4340, Aug. 1998.
-
(1998)
AIAA Paper
, vol.CP-98-4340
-
-
-
59
-
-
4344713197
-
Aerodynamic parameters of High Angle-of-Attack Research Vehicle (HARV) estimated from flight data
-
Aug.
-
Klein, V., Ratvasky, T. P., and Cobleigh, B. R., "Aerodynamic Parameters of High Angle-of-Attack Research Vehicle (HARV) Estimated from Flight Data," NASA TM-102692, Aug. 1990.
-
(1990)
NASA TM-102692
-
-
Klein, V.1
Ratvasky, T.P.2
Cobleigh, B.R.3
-
60
-
-
3743088053
-
Thrust vectoring on the NASA F-18 high alpha research vehicle
-
Nov.
-
Bowers, A. H., and Pahle, J. W., "Thrust Vectoring on the NASA F-18 High Alpha Research Vehicle," NASA TM-4771, Nov. 1996.
-
(1996)
NASA TM-4771
-
-
Bowers, A.H.1
Pahle, J.W.2
-
61
-
-
84888945160
-
-
McDonnell Aircraft Co., McDonnell Douglas Corp., MDC A8575, St. Louis, MO
-
"F/A-18 Basic Aerodynamic Data," McDonnell Aircraft Co., McDonnell Douglas Corp., MDC A8575, St. Louis, MO, 1984.
-
(1984)
F/A-18 Basic Aerodynamic Data
-
-
-
62
-
-
84888975874
-
-
McDonnell Aircraft Co., McDonnell Douglas Corp., MDC A7247, Rev. B, St. Louis, MO, Nov.
-
Pelikan, R. J., and Swingle, R. L., "F/A-18 Stability and Control Data Report," McDonnell Aircraft Co., McDonnell Douglas Corp., Vols. I and II, MDC A7247, Rev. B, St. Louis, MO, Nov. 1982.
-
(1982)
F/A-18 Stability and Control Data Report
, vol.1-2
-
-
Pelikan, R.J.1
Swingle, R.L.2
-
63
-
-
4344630978
-
Results from F-18B stability and control parameter estimation flight tests at high dynamic pressures
-
Nov.
-
Moes, T. R., Noffz, G. K., and Iliff, K. W., "Results From F-18B Stability and Control Parameter Estimation Flight Tests at High Dynamic Pressures," NASA TP-2000-209033, Nov. 2000.
-
(2000)
NASA TP-2000-209033
-
-
Moes, T.R.1
Noffz, G.K.2
Iliff, K.W.3
-
64
-
-
84867817642
-
-
Rockwell International, Space Div., Downey, CA, SD71-5H-0060 Rev. M, Downey, CA, Nov.
-
"Aerodynamic Design Data Book Orbiter Vehicle STS-1," Rockwell International, Space Div., Downey, CA, SD71-5H-0060 Rev. M, Downey, CA, Nov. 1980.
-
(1980)
Aerodynamic Design Data Book Orbiter Vehicle STS-1
-
-
-
65
-
-
84888967119
-
Correlation of predicted and flight determined stability and control derivatives-with particular application to tailless delta wing configurations
-
July
-
Weil, J., and Powers, B. G., "Correlation of Predicted and Flight Determined Stability and Control Derivatives-with Particular Application to Tailless Delta Wing Configurations," NASA TM-81361, July 1981.
-
(1981)
NASA TM-81361
-
-
Weil, J.1
Powers, B.G.2
-
66
-
-
85006415905
-
Shuttle entry aerothermodynamic flight research: The Orbiter Experiments (OEX) Program
-
July
-
Throckmorton, D. A., "Shuttle Entry Aerothermodynamic Flight Research: The Orbiter Experiments (OEX) Program," AIAA Paper CP-92-3987, July 1992.
-
(1992)
AIAA Paper
, vol.CP-92-3987
-
-
Throckmorton, D.A.1
|