Abstract

1 Cannon, R. H., Jr., Alignment of inertial guidance systems by gyrocompassing—linear theory, J. Aerospace Sci. 28, 885895,912(1961). 2 McMurray, L. R., Alignment of an inertial autonavigator, ARSJ.31,356-360(1961). 3 Narendra, K. S., Pole-zero configurations and transient response of linear systems/' TR-299, Cruft Lab., Harvard Univ. (May 1959). 4 Draper, C. S., McKay, W., and Lees, S., Instrument Engineering (McGraw-Hill Book Co. Inc., New York, 1953), Vol. 2, p.265. 5 Newton, G. C., Jr., Gould, L. A., and Kaiser, J. F., Analytical Design of Linear Feedback Controls (John Wiley and Sons, Inc., New York, 1957), Appendix E, pp. 366-381. 6 Roitenberg, I. N., The accelerated placing of a gyroscopic compass in a meridian, J. Appl. Math. Mech. 23, no. 5, 13701374 (1959). 7 Friedman, A. L., The use of speed and position fix information in inertial navigators, ARS Preprint 1957-61 (August 1961). 8 Gelb, A. and Sandberg, H. J., Finding system settling time, Control Eng. 9, 103-104 (November 1962). 9 Pitman, G. R., Jr., Inertial Guidance (John Wiley and Sons, Inc., New York, 1962), Chap. 8, pp. 176-209.

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