Show simple item record

contributor authorDavid C. Zimmerman
date accessioned2017-05-08T21:15:45Z
date available2017-05-08T21:15:45Z
date copyrightJanuary 1993
date issued1993
identifier other%28asce%290893-1321%281993%296%3A1%2876%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44760
description abstractSimultaneous design of a structure/active control system in which the mass of the actuators required to implement the active control is considered is addressed. The inclusion of required actuator mass essentially tightens the coupling between structure and control dynamics and introduces an inner iteration loop in the overall design process. Because this inner iteration loop significantly increases the computational burden, an algorithm for estimating the required actuator mass, given the control law and the desired maneuver, is presented. Additionally, a secant‐based actuator mass update algorithm is investigated in order to improve convergence characteristics of the inner iteration loop. A nonlinear optimization algorithm is used to direct the design process. The methodology is demonstrated on the design of a large two‐dimensional L‐shaped structure in which it is desired to minimize the line‐of‐sight‐pointing error between the two ends of the L after a worst‐case slew maneuver.
publisherAmerican Society of Civil Engineers
titleStructure/Control Synthesis with Nonnegligible Actuator Mass
typeJournal Paper
journal volume6
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1993)6:1(76)
treeJournal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record