1979
DOI: 10.1109/tsmc.1979.4310229
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Applied Optimal Control: Optimization, Estimation, and Control

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Cited by 630 publications
(439 citation statements)
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“…The minimisation of errors through gradient descent (Hadamard, 1908) in the parameter space of complex, nonlinear, differentiable (Leibniz, 1684), multi-stage, NN-related systems has been discussed at least since the early 1960s (e.g., Kelley, 1960;Bryson, 1961;Bryson and Denham, 1961;Pontryagin et al, 1961;Dreyfus, 1962;Wilkinson, 1965;Amari, 1967;Bryson and Ho, 1969;Director and Rohrer, 1969), initially within the framework of Euler-LaGrange equations in the Calculus of Variations (e.g., Euler, 1744).…”
Section: -1981 and Beyond: Development Of Backpropagation (Bp) Fomentioning
confidence: 99%
See 1 more Smart Citation
“…The minimisation of errors through gradient descent (Hadamard, 1908) in the parameter space of complex, nonlinear, differentiable (Leibniz, 1684), multi-stage, NN-related systems has been discussed at least since the early 1960s (e.g., Kelley, 1960;Bryson, 1961;Bryson and Denham, 1961;Pontryagin et al, 1961;Dreyfus, 1962;Wilkinson, 1965;Amari, 1967;Bryson and Ho, 1969;Director and Rohrer, 1969), initially within the framework of Euler-LaGrange equations in the Calculus of Variations (e.g., Euler, 1744).…”
Section: -1981 and Beyond: Development Of Backpropagation (Bp) Fomentioning
confidence: 99%
“…Steepest descent in the weight space of such systems can be performed (Bryson, 1961;Kelley, 1960;Bryson and Ho, 1969) by iterating the chain rule (Leibniz, 1676;L'Hôpital, 1696)à la Dynamic Programming (DP) (Bellman, 1957). A simplified derivation of this backpropagation method uses the chain rule only (Dreyfus, 1962).…”
Section: -1981 and Beyond: Development Of Backpropagation (Bp) Fomentioning
confidence: 99%
“…First-order necessary conditions for optimality are given by the Pontryagin Maximum Principle [23,5]. It can easily be shown that extremals are normal (in the sense of optimal control) and therefore these conditions reduce to the following statement: If u * is an optimal control with corresponding trajectory (N * , c * ), then there exists an absolutely continuous function (λ, µ), which we write as row-vectors λ :…”
Section: Necessary Conditions For Optimalitymentioning
confidence: 99%
“…In principle, this order can vary with time over the interval I. If it is constant on the interval I, then it is a necessary condition for optimality of a singular arc of order k, the so-called generalized Legendre-Clebsch condition [12,5], that…”
Section: Singular Extremalsmentioning
confidence: 99%
“…On the other hand, modern guidance laws are developed based on optimal control [19], [11], sliding mode control [20], differential geometry [21], and so on. Interestingly, in a linearized engagement geometry against a moving but non-maneuvering target, TPN was shown to be optimal in [22]. And, for aerodynamically driven vehicles like fixed-wing UAVs PPN is more suited option than TPN.…”
Section: Introductionmentioning
confidence: 99%