scholarly journals Abstraction Predictive Control for Chaotic Spacecraft Orbit Design**This work was supported by a NASA Space Technology Research Fellowship, grant #NNX12AM40H.

2015 ◽  
Vol 48 (23) ◽  
pp. 178-184
Author(s):  
David A Surovik ◽  
Daniel J Scheeres
Author(s):  
Adam W. Koenig ◽  
Simone D'Amico ◽  
Eliad Peretz ◽  
Wayne Yu ◽  
Sun Hur-Diaz ◽  
...  

2011 ◽  
Vol 19 (1) ◽  
pp. 1-23 ◽  
Author(s):  
Gregory. S. Hornby ◽  
Jason D. Lohn ◽  
Derek S. Linden

Whereas the current practice of designing antennas by hand is severely limited because it is both time and labor intensive and requires a significant amount of domain knowledge, evolutionary algorithms can be used to search the design space and automatically find novel antenna designs that are more effective than would otherwise be developed. Here we present our work in using evolutionary algorithms to automatically design an X-band antenna for NASA's Space Technology 5 (ST5) spacecraft. Two evolutionary algorithms were used: the first uses a vector of real-valued parameters and the second uses a tree-structured generative representation for constructing the antenna. The highest-performance antennas from both algorithms were fabricated and tested and both outperformed a hand-designed antenna produced by the antenna contractor for the mission. Subsequent changes to the spacecraft orbit resulted in a change in requirements for the spacecraft antenna. By adjusting our fitness function we were able to rapidly evolve a new set of antennas for this mission in less than a month. One of these new antenna designs was built, tested, and approved for deployment on the three ST5 spacecraft, which were successfully launched into space on March 22, 2006. This evolved antenna design is the first computer-evolved antenna to be deployed for any application and is the first computer-evolved hardware in space.


2000 ◽  
Author(s):  
John Stubstad ◽  
Richard J. Blott ◽  
James Shoemaker

1998 ◽  
Vol 35 (5) ◽  
pp. 647-652 ◽  
Author(s):  
I. L. Harris ◽  
A. R. Chambers ◽  
G. T. Roberts

Author(s):  
K Ryden ◽  
D G Fearn ◽  
R D Gould

In order to test in orbit a wide variety of new systems and technologies and to carry out associated research, the Royal Aerospace Establishment is developing two small 50 kg satellites, designated Space Technology Research Vehicles 1a and 1b. They are scheduled to be launched into the geostationary transfer orbit by an Ariane 4 in 1993; in this orbit they will be able to investigate the effects of a very high radiation dose, atomic oxygen erosion and spacecraft charging. The paper discusses the design of the spacecraft and describes the development status as at September 1991. Details are also given of a selection of the payload experiments.


1993 ◽  
Author(s):  
Keith A. Ryden ◽  
D. G. Fearn ◽  
Syl H. Alexander

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