Hostname: page-component-78c5997874-94fs2 Total loading time: 0 Render date: 2024-11-09T09:07:13.908Z Has data issue: false hasContentIssue false

Some Problems in the Navigation of Supersonic Aircraft

Published online by Cambridge University Press:  18 January 2010

W. L. Polhemus
Affiliation:
(University of Michigan)

Abstract

This paper, which was presented at a meeting of the Deutsche Gesellschaft für Ortung und Navigation held in Berlin on 24 April 1963, briefly discusses some of the factors which will affect navigation and control of supersonic transport aircraft. Attention is directed to the special problems of determining optimum flight path and estimating position and E.T.A. during three phases of the flight: acceleration, supersonic cruise and deceleration.

Type
Research Article
Copyright
Copyright © The Royal Institute of Navigation 1963

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1Polhemus, W. L. (1962). Special report from I.O.N. S.S.T. Advisory Committee Meeting of 12 September 1961.Google Scholar
2Aviation Week Magazine, 1 April 1963.Google Scholar
3Serebreny, S. M. (1963). Meteorological factors of supersonic transport operation, Navigation, The Journal of the American Institute of Navigation, 10, 57.CrossRefGoogle Scholar
4Tewles, S. (1958). Anomalous warming of the stratosphere over North Atlantic in early 1957, U.S. Weather Bureau Monthly Weather Review, 86, 377.2.0.CO;2>CrossRefGoogle Scholar
5Eberhard, R. C. (1962). The B-58 navigation system, the capabilities of a sophisticated, high speed navigation system, Navigation, Journal of the French Institute of Navigation, 10, 115.Google Scholar
6Polhemus, W. L. (1960). Navigation of the supersonic B-58. This Journal, 13, 406.Google Scholar
7MacFarland, R. A. (1953). Human factors in air transportation, McGraw-Hill Book Company, Inc. 1953. Chap. 15, 673721.Google Scholar
8Del Vecchio, R. J. (1963). Passenger tolerance to transverse acceleration and deceleration forces. A memorandum between Del Vecchio of Grumman Aircraft Co. and Hageman of G/D, Fort Worth.Google Scholar

BIBLIOGRAPHY

1Power, J. K. (1961). Some Considerations of Sonic Boom, a study conducted by the F.A.A., Office of Plans.Google Scholar
2Power, J. K. (1963). Aircraft performance factors affecting S.S.T. operation in the horizontal and vertical planes, Navigation, Los Angeles, 10, 29.Google Scholar
3Hooton, E. N. (1962). An Analysis of Three-Dimensional Navigation and Traffic Control in the Terminal Area (Slant Airways). Report No. 8420-1. Contract FAA/BRD-357.Google Scholar
4Richardson, D. W. (1963). The central electronic management system: facts and future for the S.S.T., Navigation, Los Angeles, 9, 305.Google Scholar
5Report of Institute of Navigation S.S.T. Advisory Committee, April 1962.Google Scholar
6Polhemus, W. L. (1962). The navigation and control of supersonic aircraft. This Journal, 11, 179.Google Scholar
7Pearson, R. G. and Swearingen, J. (1963). ‘Some Comments on g accelerations on Passengers.’ A letter from C.A.R.I., F.A.A., Oklahoma City.Google Scholar