Shape determination of large deployable space structures through the use of fiber-optics with integrated fiber-Bragg's gratings

2007 ◽  
Author(s):  
Brandon J. Arritt ◽  
Charles Klimcak ◽  
Eric Pollard ◽  
Hans-Peter Dumm ◽  
Thomas Murphey
2010 ◽  
Vol 6 ◽  
pp. 10004
Author(s):  
M. Francois ◽  
B. Semin ◽  
H. Auradou ◽  
J. Vatteville

2020 ◽  
Author(s):  
Haohang Huang ◽  
◽  
Jiayi Luo ◽  
Erol Tutumluer ◽  
John Hart ◽  
...  

2001 ◽  
Vol 12 (1) ◽  
pp. 87-94 ◽  
Author(s):  
Clara E. Huisinga-Fischer ◽  
Frans W. Zonneveld ◽  
J. Michiel Vaandrager ◽  
Birte Prahl-Andersen ◽  
Barry L. Eppley

1984 ◽  
Vol 106 (4) ◽  
pp. 267-272 ◽  
Author(s):  
Connie J. Weeks

An integral operator approach is used to derive solutions to static shape determination and control problems associated with large space structures. Problem assumptions include a linear self-adjoint system model, observations and control forces at discrete points, and quadratic performance criteria for the comparison of estimates or control forces. Solutions reduce to the solution of linear equations of dimension on the order of the numbers of observations or control forces. Results are illustrated by simulations with a finite element model of a large space antenna. Modal expansions for terms in the solution algorithms are presented, using modes from the static or associated dynamic model. These expansions provide approximate solutions in the event that a closed form analytical solution to the system boundary value problem is not available.


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