Storming Media: Pentagon Reports and DocumentsPentagon Reports: Fast. Definitive. Complete.     
New Account »
Forgot Password?
Advanced Search »

Newsletter
Unsubscribe »
Reports by Author

J. V. Breakwell


Click on the titles below to find US government-authored or -collected reports written by J. V. Breakwell

Total Results: 4 Results per page:
Sort by: Title Date Desc Pages Display:
The Variable-Speed Tail-Chase Aerial Combat Problem. MAY 1981
Authors:  B. S. A. Jarmark; A. W. Merz; J. V. Breakwell; SAAB-SCANIA A B LINKOPING (SWEDEN)*
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.


Study to Develop Gradiometer Techniques, JAN 1979
Authors:  D. B. DeBra; J. V. Breakwell; M. Kurosaki; STANFORD UNIV CALIF GUIDANCE AND CONTROL LAB
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.This report is concerned with the problem of real-time filtering of gravity-gradiometer readings onboard a uniformly horizontally moving vehicle to produce estimates of the gravity deflection and gravity anomaly at the vehicle's position. (Author)


ON THE CONJUGATE POINT CONDITION FOR THE CONTROL PROBLEM. 26 MAR 1964
Authors:  J. V. Breakwell; Yu-Chi Ho; HARVARD UNIV CAMBRIDGE MASS CRUFT LAB
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.In this report the conjugate point condition was derived in the classical calculus of variations from a control-theoretic point of view. The relationship of conjugate point condition to relative minimum in optimal control problem was discussed. (Author)


ACCURACY OF ORBIT DETERMINATION. OCT 1960 24 pages
Authors:  J. V. Breakwell; LOCKHEED MISSILES AND SPACE CO SUNNYVALE CALIF
The full text of this report is available for sale.This report describes a computational program, now in existence, for estimating the accuracy with which satellite positions can be calculated at any time on the basis of observations at various stations. The error in computed position is due to two main causes, at least if station location uncertainties are ignored. These are: (A) observation errors, (B) fluctuations in the orbital decay rate due to drag. It is assumed here that ...


Total Results: 4 Results per page: