Allocation of DSST in the New implementation of Tastrodyweb Tools Web-site
Abstract
The Draper Semianalytic Satellite Theory (DSST) is a semianalytic orbit propagator, which was carried out on Fortran to run from a command line interface. The construction of DSST began at the Computer Sciences Corporation and continued at the Draper Laboratory in the late 1970's and early 1980's. There are two versions of this application. One of them can be found as an option within the Goddard Trajectory Determination System (GTDS), whereas the other is available as a Standalone Orbit Propagator Package. Both versions are constantly evolving and updating. This constant evolution and updating allows DSST to take into account a wide variety of perturbation forces, which can be selected by means of a non-trivial options system at run time, and makes DSST a useful tool for performing short-term high accuracy orbit determination as well as long-term evolution. DSST has been included as part of an open source project for Space Situational Awareness and space object catalog work. On the last IAC 2011 a first step was taken in this sense and DSST was included on the tastrody Web-Site prototype [3, 4], which provided DSST with a friendly web interface, thus simplifying its use for both expert and non-expert users. However, this prototype has evolved into a stable platform based on the Drupal open source content management system (http://drupal.org Drupal), which simplifies the integration of our own application server. Drupal is supported by a large group of developers and users. Furthermore, a significant number of web-sites have been created using Drupal. In this work we present the integration of DSST in the new web-site, the new facilities provide by this platform to create the research community based on DSST and the comparison tests between the GTDS DSST, DSST Standalone and DSST Web version. These tests will be available in order to facilitate the user with better understanding of DSST.
REFERENCES [1] J. G. Neelon, P. J. Cefola, and R. J. Proulx, Current Development of the Draper Semianalytical Satellite Theory Standalone Orbit Propagator Package", AAS Pre-print 97-731, presented at the AAS/AIAA Astrodynamics Conference, Sun Valley, ID, August 1997. [2] P. J. Cefola, D. Phillion, and K. S. Kim, Improving Access to the Semi-Analytical Satellite Theory, AAS 09-341, presented at the AAS/AIAA Astrodynamic Specialist Conference, Pittsburgh, PA, August 2009. [3] P. J. Cefola, B. Weeden and C. Levit, Open Source Software Suite for Space Situational Awareness and Space Object Catalog Work, 4th International Conference on Astrodynamics Tools Techniques, Madrid, Spain, 3-6 May 2010. [4] J. F. San Juan, R. López and I. Pérez, Nonlinear Dynamics Web Tools, 4th International Conference on Astrodynamics Tools Techniques, Madrid, Spain, 3-6 May 2010. [5] J. F. San Juan, M. Lara, R. López. L. M. López, B. Weeden and P. J. Cefola, Using the DSST Semi-Analytical Orbit. Propagator Package via the NondyWebTools/. AstrodyWebTools. Proceedings of 62nd International Astronautical Congress, Cape Town, SA., 2011.- Publication:
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Advanced Maui Optical and Space Surveillance Technologies Conference
- Pub Date:
- September 2012
- Bibcode:
- 2012amos.confE..47S