Oldenburger, Rufus 1908
Overview
Works:  26 works in 87 publications in 2 languages and 1,340 library holdings 

Genres:  Conference proceedings 
Roles:  Author, Editor 
Classifications:  TJ213, 629.8 
Publication Timeline
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Most widely held works by
Rufus Oldenburger
Mathematical engineering analysis
by
Rufus Oldenburger(
Book
)
21 editions published between 1944 and 1990 in English and Undetermined and held by 392 WorldCat member libraries worldwide
21 editions published between 1944 and 1990 in English and Undetermined and held by 392 WorldCat member libraries worldwide
Frequency response
by
Rufus Oldenburger(
Book
)
14 editions published between 1954 and 1956 in English and Undetermined and held by 304 WorldCat member libraries worldwide
14 editions published between 1954 and 1956 in English and Undetermined and held by 304 WorldCat member libraries worldwide
Optimal and selfoptimizing control
by
Rufus Oldenburger(
Book
)
6 editions published in 1966 in English and held by 273 WorldCat member libraries worldwide
6 editions published in 1966 in English and held by 273 WorldCat member libraries worldwide
Optimal control
by
Rufus Oldenburger(
Book
)
11 editions published between 1966 and 1968 in English and held by 245 WorldCat member libraries worldwide
11 editions published between 1966 and 1968 in English and held by 245 WorldCat member libraries worldwide
Symbolic dynamics : lectures by Marston Morse 19371938
by
Marston Morse(
Book
)
4 editions published between 1966 and 1974 in English and held by 30 WorldCat member libraries worldwide
4 editions published between 1966 and 1974 in English and held by 30 WorldCat member libraries worldwide
Optimum nonlinear control of a second order nonlinear system
by
Rufus Oldenburger(
Book
)
4 editions published in 1961 in English and held by 24 WorldCat member libraries worldwide
4 editions published in 1961 in English and held by 24 WorldCat member libraries worldwide
Selfoscillations in sampleddata systems with saturation
by
Rufus Oldenburger(
Book
)
2 editions published in 1966 in English and held by 21 WorldCat member libraries worldwide
2 editions published in 1966 in English and held by 21 WorldCat member libraries worldwide
Symbolic dynamics; lectures by Marston Morse, 193738
by
Marston Morse(
Book
)
3 editions published in 1966 in English and held by 13 WorldCat member libraries worldwide
3 editions published in 1966 in English and held by 13 WorldCat member libraries worldwide
Composition and rank of nway matrices and multilinear forms
by
Rufus Oldenburger(
Book
)
4 editions published in 1934 in English and held by 10 WorldCat member libraries worldwide
4 editions published in 1934 in English and held by 10 WorldCat member libraries worldwide
Symbolic dynamics : lectures, 19371939
by
Marston Morse(
Book
)
1 edition published in 1966 in English and held by 10 WorldCat member libraries worldwide
1 edition published in 1966 in English and held by 10 WorldCat member libraries worldwide
Kōgaku mondai no kaiseki
(
Book
)
2 editions published in 1956 in Japanese and held by 3 WorldCat member libraries worldwide
2 editions published in 1956 in Japanese and held by 3 WorldCat member libraries worldwide
Symbolic dynamics
by
Marston Morse(
Book
)
1 edition published in 1966 in English and held by 1 WorldCat member library worldwide
1 edition published in 1966 in English and held by 1 WorldCat member library worldwide
TIME OPTIMAL CONTROL FOR A CLASS OF COMMON RANDOM DISTURBANCES
(
Book
)
1 edition published in 1970 in English and held by 1 WorldCat member library worldwide
The paper concerns the time optimal control of a system variable where the controlling input is bounded, as is usually the case, and the system is subject to arbitrary disturbances. An arbitrary disturbance is made up of uncontrollable portions followed by controllable sections. In industrial practice controllers are sized, as for example as to power, to fit the system so that the disturbances encountered are primarily made up of uncontrollable sections followed by controllable portions of sufficient duration for the controller to bring the system equilibrium. The control designer wishes to have optimal control for any disturbance made up of such an uncontrollable portion followed by a sufficiently long controllable section. Here this problem is solved with the aid of the maximum principle for the class of second order systems which describe almost all governorengine applications to first approximation accuracy. Previous attempts to solve the problem involved assuming statistical properties of the disturbance thus severely restricting the class of applications. Here only those statistical properties required to implement optimal control are determined. A single control function is derived which suffices to yield optimal trajectories. (Author)
1 edition published in 1970 in English and held by 1 WorldCat member library worldwide
The paper concerns the time optimal control of a system variable where the controlling input is bounded, as is usually the case, and the system is subject to arbitrary disturbances. An arbitrary disturbance is made up of uncontrollable portions followed by controllable sections. In industrial practice controllers are sized, as for example as to power, to fit the system so that the disturbances encountered are primarily made up of uncontrollable sections followed by controllable portions of sufficient duration for the controller to bring the system equilibrium. The control designer wishes to have optimal control for any disturbance made up of such an uncontrollable portion followed by a sufficiently long controllable section. Here this problem is solved with the aid of the maximum principle for the class of second order systems which describe almost all governorengine applications to first approximation accuracy. Previous attempts to solve the problem involved assuming statistical properties of the disturbance thus severely restricting the class of applications. Here only those statistical properties required to implement optimal control are determined. A single control function is derived which suffices to yield optimal trajectories. (Author)
Riemann surfaces for equations x('n) + y('n) = r('n)
by
Rufus Oldenburger(
)
1 edition published in 1930 in English and held by 1 WorldCat member library worldwide
1 edition published in 1930 in English and held by 1 WorldCat member library worldwide
Theory of distributed systems
by
Rufus Oldenburger(
Book
)
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
QUENCHING OF ADAPTIVE CONTROL SYSTEM RESPONSE TO TEST SIGNAL
(
)
1 edition published in 1962 in English and held by 1 WorldCat member library worldwide
1 edition published in 1962 in English and held by 1 WorldCat member library worldwide
Time optimal control for a class of common random disturbances
by
Rufus Oldenburger(
Book
)
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
ADAPTIVE AND SELFOPTIMIZING CONTROL
(
Book
)
1 edition published in 1970 in English and held by 1 WorldCat member library worldwide
The final report summarizes the research accomplished on the contract by reference listing with appropriate abstracts the publications, books, technical reports, and theses completed under contract support. (Author)
1 edition published in 1970 in English and held by 1 WorldCat member library worldwide
The final report summarizes the research accomplished on the contract by reference listing with appropriate abstracts the publications, books, technical reports, and theses completed under contract support. (Author)
Identification of impulse response from normal operating data using the delay line synthesizer principle
(
Book
)
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
A computational technique is presented for identifying the impulse response of a linear system from normal operating noisy data. No assumption, however, is made regarding the nature of the noise. The technique derives its idea from the Delay Line Synthesizer (DLS) though in this case the DLS coefficients which discretely represent the weighing function are computed automatically employing the steepest descent method. The method has been tried out on a first order as well as a second order system simulated on a digital computer and the estimated impulse response is found to be very close to the actual one. (Author)
1 edition published in 1969 in English and held by 1 WorldCat member library worldwide
A computational technique is presented for identifying the impulse response of a linear system from normal operating noisy data. No assumption, however, is made regarding the nature of the noise. The technique derives its idea from the Delay Line Synthesizer (DLS) though in this case the DLS coefficients which discretely represent the weighing function are computed automatically employing the steepest descent method. The method has been tried out on a first order as well as a second order system simulated on a digital computer and the estimated impulse response is found to be very close to the actual one. (Author)
SELECTION OF A DELAY LINE MODEL
(
Book
)
1 edition published in 1964 in English and held by 1 WorldCat member library worldwide
A mathematical model of a linear system can be derived using an approximation of the convolution integral. A model is selected such that responses to commonly occurring inputs are closest to corresponding responses of the system. The transfer function of the model is the product of the system transfer function by a linear combination of two delay terms divided by an infinite product. If the model delay time is small the infinite product may be replaced by 1, and thus may be dropped. The delay time and the number of delay elements are selected such that the responses of the simplified model are closest to corresponding responses of the system. The validity of the simplification is investigated for various inputs by comparing the responses of the simplified model with those of the exact model. It is found for several types of commonly occurring inputs that the number of delay elements should be chosen as large as physically possible. The results show that the value of the delay time should be selected as a function of the number of delay elements and of the system bandwidth. It is further shown that this function is the same for each of the inputs
1 edition published in 1964 in English and held by 1 WorldCat member library worldwide
A mathematical model of a linear system can be derived using an approximation of the convolution integral. A model is selected such that responses to commonly occurring inputs are closest to corresponding responses of the system. The transfer function of the model is the product of the system transfer function by a linear combination of two delay terms divided by an infinite product. If the model delay time is small the infinite product may be replaced by 1, and thus may be dropped. The delay time and the number of delay elements are selected such that the responses of the simplified model are closest to corresponding responses of the system. The validity of the simplification is investigated for various inputs by comparing the responses of the simplified model with those of the exact model. It is found for several types of commonly occurring inputs that the number of delay elements should be chosen as large as physically possible. The results show that the value of the delay time should be selected as a function of the number of delay elements and of the system bandwidth. It is further shown that this function is the same for each of the inputs
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Associated Subjects
Automatic control Discretetime systems Dynamics Engineering mathematics Forms (Mathematics) Frequency response (Dynamics) Geometry, Projective Laplace transformation Matrices Mechanics, Applied Nonlinear control theory Oscillations Pipelines Realtime control Riemann surfaces Servomechanisms Stability Topological dynamics Vibration