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Author: L. E. Ericsson Publisher: ISBN: Category : Languages : en Pages : 22
Book Description
The aerodynamic information needed for preliminary design of tactical missiles has always been obtained through the combined use of theory and experiments. In regard to the static aerodynamics this has resulted in a prediction capability that often is satisfactory for preliminary design. However, the vehicle dynamics cannot be predicted with the same confidence, especially not at the high angles of attack where high performance missiles often must operate. In this case we are still dependent upon continuous efficient interaction between theoretical and experimental methods. The paper delineats the limitations of both methods and describes how to circumvent them in order to predict tactical missile dynamics over the required range of operational parameters. (JES).
Author: L. E. Ericsson Publisher: ISBN: Category : Languages : en Pages : 22
Book Description
The aerodynamic information needed for preliminary design of tactical missiles has always been obtained through the combined use of theory and experiments. In regard to the static aerodynamics this has resulted in a prediction capability that often is satisfactory for preliminary design. However, the vehicle dynamics cannot be predicted with the same confidence, especially not at the high angles of attack where high performance missiles often must operate. In this case we are still dependent upon continuous efficient interaction between theoretical and experimental methods. The paper delineats the limitations of both methods and describes how to circumvent them in order to predict tactical missile dynamics over the required range of operational parameters. (JES).
Author: American Institute of Aeronautics and Astronautics Publisher: AIAA (American Institute of Aeronautics & Astronautics) ISBN: 9781563470165 Category : Science Languages : en Pages : 806
Book Description
Prediction Methodology contains updated versions of nine chapters from the first edition and chapters on drag prediction, component build-up methods, Euler methods and Navier-Stokes solvers. Special attention is paid to nonlinear flow phenomena and unconventional airframe shapes. Eight colour plates and more than 540 figures are included.
Author: Qi Zaikang Publisher: CRC Press ISBN: 1000680673 Category : Technology & Engineering Languages : en Pages : 255
Book Description
Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.
Author: Eugene L. Fleeman Publisher: AIAA (American Institute of Aeronautics & Astronautics) ISBN: Category : Technology & Engineering Languages : en Pages : 298
Book Description
This is the first textbook offered for tactical missile design. It is oriented toward the needs of aerospace engineering students, missile engineers, and missile program managers. It is intended to provide a basis for including tactical missile design as part of the aerospace engineering curriculum, providing new graduates with the knowledge they will need in their careers. The author's decades of experience in the development of tactical missiles and their technologies is presented in an integrated handbook method for missile design. It uses simple closed-form analytical expressions that are physics-based to provide insight into the primary driving parameters. The text also provides example calculations of rocket-powered and ramjet-powered baseline missiles, typical values of missile parameters, examples of the characteristics of current operational missiles, discussion of the enabling subsystems and technologies of tactical missiles, and the current/projected state of the art of tactical missiles. Included with the text is a CD-ROM containing electronic versions of the figures; 15 videos showing examples of loading missiles, pilot actions, flight trajectories, countermeasures, etc.; and configuration sizing methods.
Author: Heinz Fuchs Publisher: ISBN: Category : Languages : en Pages : 19
Book Description
The prediction methodology of dynamic derivatives is presented as derived from semiempirical calculation procedures like 'USAF Stability and Control Datcom' in combination with some modifications necessary for tactical missile configurations at higher angles-of-attack. The main subject is the longitudinal stability derivatives and the roll damping derivativum. A comparison of theoretical and experimental results is presented where different dynamic wind tunnel test equipments are explained including the data evaluation theory. Some aspects of modification of the present linear data evaluation method to nonlinear terms at high angles-of-attack are shown with an example of a fighter aircraft configuration using the MOD test rig in the Dornier wind tunnel. Guided missiles, Aerodynamics. (JES).
Author: N A Shneydor Publisher: Elsevier ISBN: 1782420592 Category : Technology & Engineering Languages : en Pages : 276
Book Description
The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. - Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer - Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process
Author: L. E. Ericsson
Author: L. E. Ericsson
Author: American Institute of Aeronautics and Astronautics
Author: M. R. Mendenhall
Author: 
Author: Qi Zaikang
Author: Eugene L. Fleeman
Author: 
Author: Heinz Fuchs
Author: N A Shneydor
Author: John Harris