Weapon Delivery Analysis and Ballistic Flight Testing
| Author | : R. J. Arnold |
| Publisher | : |
| Total Pages | : 176 |
| Release | : 1992 |
| Genre | : Ballistics |
| ISBN | : |
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Weapon Delivery Analysis And Ballistic Flight Testing
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AGARD Flight Test Techniques Series
| Author | : R.J.. Arnold |
| Publisher | : |
| Total Pages | : |
| Release | : 1992 |
| Genre | : |
| ISBN | : 9789283506775 |
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AGARD Flight Test Series. Volume 10. Weapon Delivery Analysis and Ballistic Flight Testing (L'Analyse Du Largage D'Armes Et Les en Vol Balistique).
| Author | : |
| Publisher | : |
| Total Pages | : 172 |
| Release | : 1992 |
| Genre | : |
| ISBN | : |
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This volume in the AGARD Flight Test Techniques series treats stores ballistic modeling/testing from the overall system standpoint. All aspects of the ballistic testing design, data collection techniques, data reduction, analysis techniques, and finally the Operational Flight Program modeling techniques are addressed. Considerable effort has been expended to keep this report straightforward so that it can be understood by management as well as engineering personnel, but with sufficient engineering principles addressed so that a true ballistician could use it from an application perspective.
AGARD Flight Test Techniques Series Volume 10 on Weapon Delivery Analysis and Ballistic Flight Testing
| Author | : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development |
| Publisher | : |
| Total Pages | : |
| Release | : 1992 |
| Genre | : |
| ISBN | : |
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Scientific and Technical Aerospace Reports
| Author | : |
| Publisher | : |
| Total Pages | : 484 |
| Release | : 1993 |
| Genre | : Aeronautics |
| ISBN | : |
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Development of Weapon Delivery Models and Analysis Programs. Volume III. Testing and Demonstration of the Armament Delivery Analysis Programming System (ADAPS).
| Author | : A. Ferit Konar |
| Publisher | : |
| Total Pages | : 194 |
| Release | : 1972 |
| Genre | : |
| ISBN | : |
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D Analysis Programs. Volume III. Testing and Demonstration of the Armament Delivery Analysis Programming System (ADAPS). Final technical rept. 5 Oct 70-5 Oct 71,FKonar, A. Ferit ;Ward, Michael D. ;12261-FRI-Vol-3F33615-71-C-1059AF-8219821904AFFDLTR-71-123-Vol-3Availability: Document partially illegible.(*close support, mathematical models), (*bomb trajectories, circular error probable), effectiveness, computer programs, flight control systems, gust loads, equations of motion, miss distance, weapon systems, partial differential equations, perturbation theory, white noise, numerical analysism-117 bombs(750-lb), adap computer program, automatic, control, bomb release point, fortran, fortran 4 programming language, f-4 aircraft, control theoryThe testing and use of ADAPS is demonstrated by performing an analysis with a specified iron bomb (M117) and a representative tactical fighter-bomber aircraft (F4). The demonstration example revealed no appreciable performance difference between the time-invariant and time-invariant and time-varying optimal controllers for the weapon delivery process. The contribution matrix of an iron bomb indicated that the major contributors to the CEP are the velocity and the attitude-state errors at release. (Author).
Introduction to Avionics Flight Test
| Author | : James M. Clifton |
| Publisher | : |
| Total Pages | : 356 |
| Release | : 1996 |
| Genre | : Airplanes, Military |
| ISBN | : |
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AGARDograph
| Author | : |
| Publisher | : |
| Total Pages | : 182 |
| Release | : 1954 |
| Genre | : Aerodynamics |
| ISBN | : |
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Analysis of Piloted Weapon Delivery: Strafing Performance of a Foreign Aircraft
| Author | : William P. Hartmann |
| Publisher | : |
| Total Pages | : 75 |
| Release | : 1972 |
| Genre | : |
| ISBN | : |
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In order to determine whether the weapon delivery accuracy of an aircraft for which the aerodynamic stability derivatives were not known could be estimated, the strafing performance of an unspecified foreign tactical fighter was analyzed. The stability derivatives were estimated from the physical characteristics of the aircraft using standard stability and control methods. Also, by the use of classical control theory, the probable control system of the aircraft was formulated. Then, with an analytical pilot model in the aircraft's control loop, the tracking error was estimated and combined with other pilot-induced errors in a statistical model which predicts impact errors. (Author).
NATO Defense and the INF Treaty
| Author | : United States. Congress. Senate. Committee on Armed Services |
| Publisher | : |
| Total Pages | : 640 |
| Release | : 1989 |
| Genre | : Europe |
| ISBN | : |
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