Reply by Authors to K. W. London

Abstract

Lips, K. W. and Modi, V. J., During Asymmetrical Deployment of Flexible Appendages, XXXIst International Astronautical Congress, International Astronautical Federation Paper 80-E-227, Sept. 1980. Lips, K. W. and Modi, V. J., Damped Response of with Flexible Deploying Appendages, Proceedings of the 3rd VPI and SU/AIAA Symposium on and Control of Large Flexible edited by L. Meirovitch, AIAA, New York, 1981, pp. 203-220. Lips, K. W. and Modi, V. J., Three-Dimensional Response Characteristics for a with Deploying Flexible Appendages, Journal of Guidance and Vol. 4, Nov.-Dec. 1981, pp. 650-656. Kane, T. R., Likins, P. W., and Levinson, D. A., Spacecraft McGraw-Hill, New York, 1983, pp. 318-332. Lips/K. W., Comment on a General Formulation for Librational of with Deploying Appendages, Journal of Guidance, and Dynamics, Vol. 9, Jan.-Feb. 1986, pp. 125-126. Gelderloos, H. C. and Lips, K. W., TREETOPS MultiFlex-Body Software Applied to an SDI Slew Actuator Study, 1988 Summer Computer Simulation Conf., Society for Computer Simulations International, San Diego, CA, Paper 349, 1988. Hodges, D. H., Proper Definition of Curvature in Nonlinear Beam Kinematics, AIAA Journal, Vol. 22, Dec. 1984, pp. 1825-1827. Modi, V. J., Attitude of Satellites with Flexible Appendages—A Brief Review, Journal of and Rockets, Vol. 11, Nov. 1974, pp. 743-751. Likins, P. W., Barbera, F. J., and Baddeley, V., Mathematical Modeling of Spinning Elastic Bodies for Modal Analysis, AIAA Journal, Vol. 11, Sept. 1973, pp. 1251-1258. Hughes, P. C., Dynamics of Flexible Spinning Spacecraft, XXIV Congress of the International Astronautical Federation, Baku, USSR, Oct. 1973. Hughes, P. C., Attitude of a Three-Axis Stabilized Satellite with a Large Flexible Solar Array, Journal of Astronautical Sciences, Vol. 20, No. 3, Nov.-Dec. 1972, pp. 166-189. Hughes, P. C., Dynamics of Flexible Space Vehicles with Active Control, Celestial Mechanics, Vol. 9, 1974, pp. 21-39. Lips, K. W., Graham, W. B., Vigneron, F. R., and Hunter, D. G., Dynamics and Control Characteristics of the 300 m Dipole Antenna/Shuttle Configuration, AIAA Astrodynamics Conference, Vail, CO, Aug. 12-14 1985; also, AAS Astrodynamics, Advances in the Astronautical Sciences, Vol. 58, edited by B. Kaufmann et al., Univelt, Inc., San Diego, CA, 1985.