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Friday, July 10, 2020 | History

1 edition of Second and third order minimum time controllers and missile adjoints found in the catalog.

Second and third order minimum time controllers and missile adjoints

Colin Roy Cooper

Second and third order minimum time controllers and missile adjoints

by Colin Roy Cooper

  • 374 Want to read
  • 27 Currently reading

Published by Naval Postgraduate School, Available from the National Technical Information Service in Monterey, Calif, Springfield, Va .
Written in English


About the Edition

The month has been spent in a series of harmonic generation experiments at increasing peak intensity and fluence. Second harmonic beam quality has been measured. Using the oscillator alone, with grating selection of the 9.55 micrometer line, the pulse train consisted of a spike containing about 10 pulses followed by a tail containing about 40 pulses. Both the spike and the tail contained approximately equal energy, the combined total going as high as 180 mJ. The crystal was located near to the plane exit mirror of the oscillator, where the near-parallel beam has a Gaussian (amplitude) spot parameter of 0.46 cm. The on-axis fluence was 0.5 J/sq. cm. and the peak intensity in the 2 nsec optical pulses was approximately 20 NW/sq. cm. The pulses were separated by 40 nsec. Energy conversion efficiency of up to 31% was recorded, with 56 mJ of second harmonic (outside the crystal) for 181 mJ of incident 9.55 micrometer radiation. The second harmonic energy depended on the 1.5 power of the fundamental in the fundamental energy range 50 mJ to 180 mJ. Time-dependent analysis showed that the conversion efficiency was close to 50% in the spike but generally less than 10% in the "tail" as expected from their intensity ratio (in the range 4:1 to 8:1).

Edition Notes

Statement Colin Roy Cooper
The Physical Object
Pagination84 p. ;
Number of Pages84
ID Numbers
Open LibraryOL25492978M

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I will describe, first, missile parts and their functions, second, missile deployment, and finally, how a missile is launched to intercept and destroy its target. Missile Parts and Their Functions. A tactical missile is from 5 to 20 feet long, 6 inches to 1 foot in diameter, and weighs from to 2, pounds. The order of operations specifies the order in which the operations in an expression should be evaluated. For example, to evaluate 12 2 5, you multiply first and then add, so the result is 2. In your text, read the rules for Order of Operations and Example A. Here is another example. EXAMPLE A Evaluate the expression 7 13 4 without a calculator File Size: KB.

Start studying WTI Control of Aircraft and Missiles. Learn vocabulary, terms, and more with flashcards, games, and other study tools. Likewise, a missile controller performs air control when he directs a surface-to-air weapons unit to engage a target. Providing real-time target information in order to support coordination and. On the LAU missile launcher, what keeps the shear pin from backing out during flight? Lock nut On AIM-9 and AIM capable rail launchers, what prevents the missile from leaving the rail if the rocket motor fires inadvertently?


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Second and third order minimum time controllers and missile adjoints by Colin Roy Cooper Download PDF EPUB FB2

Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection Second and third order minimum time controllers and missile adjoints. Energy conversion efficiency of up to 31% was recorded, with 56 mJ of second harmonic (outside the crystal) for mJ of incident micrometer radiation.

The second harmonic energy depended on the power of the fundamental in the fundamental energy range 50 mJ to : Colin Roy Cooper. Similar to the 1 other review this book has a lot of good technical meat for a book on missile guidance and control (i.e., mechanics, dynamics, etc.).

This book especially has a lot of material on inertial guidance. However, there is only the most basic coverage of interceptor missile challenges and issues (my biggest area of concern).Cited by: Compared to PID controller which has Tr=0, Ts=0, %OS=3,9% umax=96% Imax=0,35 A in no load condition, proposed controller has a better settling time, control signal and current.

Though originally inspired by military applications, the advent of missile guidance and control systems has led to applications in a variety of fields -- in robotics, industrial process control, and in commercial transportation networks such as Global Positioning System technology.

This book offers a comprehensive and up-to-date account of the technology behind tactical and strategic missiles 5/5(1). The primary goal of this work is to develop the enabling guidance and control technology for missile interceptors to achieve the hit-to-kill accuracy against targets performing evasive maneuvers including spiralling motion, using high order sliding mode control (HOSM) developed in works of Floquet, Barbot, & Perruquetti (), Fridman ( Cited by: 8.

Novel smooth second-order sliding mode (SSOSM) control is studied and its finite-time convergence proved using homogeneity-based technique for a system driven by sufficiently smooth uncertain disturbances. SSOSM control was applied to designing the guidance law for the missile-interceptor against a target performing evasive by: The smooth second-order sliding mode control-based guidance law is designed and compared with augmented proportional navigation guidance law via computer simulations of a guided missile.

Section with more than 90 different optimal control problems in various categories. Air University Press (AU Press) is the publishing agent for Air University (AU). Sinceit has edited, published, and distributed over million student papers, curriculum texts, faculty research pieces, journals, and scholarly books to further airpower thought critical to the intellectual growth of the Air Force.

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Space Defense: Management and Technical Problems Delay Operations Center AcquisitionAuthor: United States General Accounting Office. Keywords: guided missile, flying body control system, Routh criterion, Root-Locus method, frequency response method. INTRODUCTION It can determine whether our design of a control system meets the specification if the desired time response of the controlled variable determined.

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Initially the Standard Missile was dual sourced between General Dynamics Pomona Division (which became part of Hughes Aircraft Company in and part of Raytheon Missile Systems Division but in.BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE INSTRUCTIONVOLUME 1 7 AUGUST Space, Missile, Command, And Control RANGE PLANNING AND OPERATIONS OPR: HQ USAF/XOOR (Lt Col Gerard Madigan/Maj Tim Brown) Certified by: HQ USAF/XOO (Maj Gen Walter E.

Buchanan III) Supersedes AFIVolume 1, 28 Jul Pages: 74 Distribution: FFile Size: KB. Step Response p=10 p=1 2 Amplitude 1 0 − p=0 (no added pole) −1 0 5 10 15 Time (sec) Figure The effect of an additional forward-path pole SummaryAs was in the case of a dominantly first-order system, the response of a dominantly second-order system is sped up by an additional zero and is slowed down by an additional.