Aerodynamic ballistic range analysis using generalized math models

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 1-11

  Yates, Leslie A ^a   Chapman, Gary T ^b,c  

^a Aerospace Computing Inc   (United States)

^b UNIVERSITY OF CALIFORNIA   (United States)

^c Department of Mechanical Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; PIECEWISE LINEAR TECHNIQUES;

AERODYNAMIC COEFFICIENT MODELS; AERODYNAMIC COEFFICIENTS; ESTIMATED ERROR; ESTIMATION APPROACHES; PIECE-WISE LINEAR FUNCTIONS; POLYNOMIAL EXPANSION; RANGE ANALYSIS; SIMULATED TRAJECTORIES;

ESTIMATION;

EID: 84983208422     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3360     Document Type: Conference Paper

References (11)

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2. Seiff, A. and Wilkins, M. E., "Experimental Investigation of a Hypersonic Glider Configuration at Mach Number 6 and Full Scale Reynolds Number," NASA TN D-341, 1961.
3. Rasmussen, M. L. and Kirk, D. B., "On the Pitching and Yawing Motion of a Spinning Projectile Governed by an Arbitrary Nonlinear Restoring Moment," NASA TN D-2135, 1964.
4. Chapman, G. T. and Kirk, D. B., "A Method for Extraction of Aerodynamic Coefficients from Free-Flight Data," AIAA J., Vol. 8, No. 4, April 1970, pp. 753-758.
5. Sabot, S. M., Winchenbach, G. L., and Chapman, G. T., "Comparison of Various Drag Coefficient Expansions Using Polynomials and Splines," J. of Spacecraft and Rockets, Vol. 23, No. 3, May-June 1986, pp. 259-263.
6. Chapman, G. T., "Ballistic Range Data Analysis Using Polynomials and Continuous and Discontinuous Splines," Proceedings of the 38th Aeroballistic Range Association Meeting, Tokyo, Japan, Oct. 5-8, 1987.
7. Chapman, G. T. and Yates, L. A., "Nonlinear Aerodynamic Parameter Estimation and Model Structure Identification," AIAA Paper 92-4502, Aug. 1992.
8. Mook, D. J., "Estimation and Identification of Nonlinear Dynamic Systems," AIAA J., Vol. 27, No. 7, July 1989, pp. 968-974.
9. Etkin, B., "Dynamics of Atmospheric Flight," John Wiley & Sons, Inc., New York, 1972.
10. Klein, V. and Batterson, J. G., "Determination of Airplane Model Structure from Flight Data using Splines and Stepwise Regression," NASA TP 2126, March 1983.
11. Dupuis, A. D. and Edwards, J., "Aerodynamic Characteristic of the CAN4 Hypersonic Research Configuration from Free-Flight Tests," DREV TM-9525, Feb. 1996.