Quantitative Assessment in Arms Control

Quantitative Assessment in Arms Control
Author: Rudolf Avenhaus
Publisher: Springer Science & Business Media
Total Pages: 472
Release: 2012-12-06
Genre: Political Science
ISBN: 1461328055

This book originates in a series of contributions to the 1983 Systems Science Seminar at the Computer Science Department of the German Armed Forces University Munich. Under the topic "Quantita tive Approaches to Arms Control" that seminar attempted to review the present state-of-the-art of systems analysis and numerate meth ods in arms control. To this end, the editors invited a number of experts from Europe, the United St~tes and Canada to share and dis cuss their views and assessments with the faculty and upper class computer science students of the university as well as numerous guests from the defence community and the interested public. In three parts, this book presents a selection of partly re vised and somewhat extended versions of the seminar presentations followed, in most cases, by brief summaries of the transcripts of the respective discussions. In addition to an introduction by the editors, part I contains six papers on the present state and prob lems of arms control with emphasis on START (Strategic Arms Re duction Talks), INF (Intermediate-range Nuclear Forces negotia tions), and MBFR (Mutually Balanced Force Reduction talks). The seven contributions to part II are devoted to mathematical models of arms competition and quantitative approaches to force balance assessment of both, the static and dynamic variety. Part III pre sents five papers which address technical and operational aspects and legal implications of arms control negotiations and verifica tion.

Two Non-linear Problems in the Flight Dynamics of Modern Ballistic Missiles

Two Non-linear Problems in the Flight Dynamics of Modern Ballistic Missiles
Author: John D. Nicolaides
Publisher:
Total Pages: 71
Release: 1958*
Genre: Ballistic missiles
ISBN:

While the linear theory has been the backbone of ballistic missile design and has served with excellent success in its various forms over the years, recent spectacular missile flight failures have appeared unexpectedly and are unaccounted for by this linear theory. It is these flight failures which now require attention and consideration of the non-linearities in the fluid force and moment system which contribute to missile flight performance and dynamic stability. Two types of non-linear flight instability have been isolated and identified as NonLinear Magnus Instability, and Catastrophic Yaw. It is these 2 flight instabilities which will be discussed. Approximate mathematical models will be suggested for the evaluation of missile dynamic stability. Both experimental and analytical applications of these models will be made and discussed.

A Mathematical Model for a Ballistic Rocket

A Mathematical Model for a Ballistic Rocket
Author: EVERETT L. WALTER
Publisher:
Total Pages: 1
Release: 1962
Genre:
ISBN:

The importance of mathematical models in designing a rocket is apparent in savings of time and money. Testing of certai theories of rocket flight can be done only by mathematical models. Such a model is given for a ballistic rocket, one for which there is no guidance after launching. It consists of six simultaneous differential equations which can be numerically solved rather quickly on a high-speed computer. All necessary parameters are completely defined, but the equations of motion are given without proof. The use of perturbation equations, which describe changes in the trajectory due to small changes in the atmospheric or rocket data, is discussed, indicating how their use can greatly increase computing speed. Numerical integration of the equations is discussed, together with the characteristics one would desire in a computer program which make the model as complete and flexible as possible. Some indication of computing speed is given, as well as the time required to program the model for a high speed computer. Finally, several applications for which the model was designed are discussed. (Author).

An Introduction to Mathematical Modeling

An Introduction to Mathematical Modeling
Author: Edward A. Bender
Publisher: Courier Corporation
Total Pages: 274
Release: 2000-03-06
Genre: Mathematics
ISBN: 9780486411804

Accessible text features over 100 reality-based examples pulled from the science, engineering and operations research fields. Prerequisites: ordinary differential equations, continuous probability. Numerous references. Includes 27 black-and-white figures. 1978 edition.

Hit-to-kill Guidance Algorithm for the Interception of Ballistic Missiles During the Boost Phase

Hit-to-kill Guidance Algorithm for the Interception of Ballistic Missiles During the Boost Phase
Author:
Publisher:
Total Pages: 141
Release: 2006
Genre: Ballistic missiles
ISBN:

A near-optimal guidance law has been developed using the direct method of calculus of variations that maximizes the kinetic energy transfer from a surface-launched missile upon interception to a ballistic missile target during the boost phase of flight. Mathematical models of a North Korean Taep'o-dong II (TD-2) medium-range ballistic missile and a Raytheon Standard Missile 6 (SM-6) interceptor are used to demonstrate the guidance law2s performance. This law will utilize the SM-62s onboard computer and active radar sensors to independently predict an intercept point, solve the two-point boundary value problem, and determine a near-optimal flight path to that point. Determining a truly optimal flight path would require significant computing power and time, while a near-optimal flight path can be calculated onboard the interceptor and updated in real time without significant changes to the interceptor2s hardware. That near-optimal guidance path is then converted into a set of command functions and fed back into the control computer of the interceptor. By modifying the second and third derivatives of the two-point boundary value problem, the intercept conditions can be varied to study their effects upon the optimal flight path regarding the maximization of kinetic energy upon impact.

OAR

OAR
Author:
Publisher:
Total Pages: 132
Release: 1963
Genre: Aeronautics
ISBN: