1980
DOI: 10.1002/oca.4660010108
|View full text |Cite
|
Sign up to set email alerts
|

Sequential conjugate gradient‐restoration algorithm for optimal control problems with non‐differential constraints and general boundary conditions, part I

Abstract: In this paper, a new member of the family of sequential gradient‐restoration algorithms for the solution of optimal control problems is presented. This is an algorithm of the conjugate gradient type, which is designed to solve two classes of optimal control problems, called Problem P1 and Problem P2 for easy indentification. Problem P1 involves minimizing a functional I subject to differential constraints and general boundary conditions. It consists of finding the state x(t), the control u(t), and the paramete… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
10
0

Year Published

1980
1980
2020
2020

Publication Types

Select...
8
1

Relationship

0
9

Authors

Journals

citations
Cited by 82 publications
(10 citation statements)
references
References 14 publications
0
10
0
Order By: Relevance
“…. The time derivative of h is described by (9) The Jacobian matrix A has dimension of 3×4 and the gimbal angular velocity vector u is the control input to the CMGs.…”
Section: Dynamics Of Satellites With Cmgsmentioning
confidence: 99%
“…. The time derivative of h is described by (9) The Jacobian matrix A has dimension of 3×4 and the gimbal angular velocity vector u is the control input to the CMGs.…”
Section: Dynamics Of Satellites With Cmgsmentioning
confidence: 99%
“…The problem is reduced to a two-point boundary-value problem (TPBVP). The authors have developed some efficient solvers for this type of problem by employing fine algorithms such as the steepest ascent method [24], the sequential conjugate gradient-restoration algorithm SCGRA [25,26], and the modified quasi-linearization algorithm MQA [27]. In this paper, the problem is solved by the STP-CODE.…”
Section: Derivation Of An Aircraft Vs Two-missiles Problemmentioning
confidence: 99%
“…Therefore it is inevitable to adopt some numerical methods to solve this problem. In this paper, the sequential conjugate gradientrestoration (SCGR) method developed by Wu and Miele (1980) was used.…”
Section: Formulationmentioning
confidence: 99%
“…Shoji and Ohtsu (1992) have formulated this problem as a nonlinear, two-point boundary value problem (TPBVP). It has been solved, using the numerical method called the sequential conjugate gradient restoration (SCGR) method (Miele & Iyer, 1970;Wu & Miele, 1980) under various situations (Ohtsu & Shoji, 1994;Ohtsu et al, 1996;Okazaki et al, 2000). However, these solutions are not suitable for online control, because it takes long computational time to obtain the optimal solution.…”
Section: Introductionmentioning
confidence: 99%