DocumentCode
3514995
Title
Implementing Plug-and-Play ADCS to Support Operationally Responsive Space
Author
Graven, Paul ; Plan, Yaniv ; Hansen, L. Jane ; Harvey, Seth
Author_Institution
Microcosm, Inc., Hawthorne, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
14
Abstract
Operationally Responsive Space (ORS)12 has become the mantra for the next generation spacecraft that will support the warfighter. ORS missions require an extension of the current, traditional approach for fine-tuned, high cost, high accuracy attitude determination and control system (ADCS) software to create an ADCS system that can be developed much faster and less expensively. To achieve this faster, cheaper, and thus, better product, new technologies must be employed. These technologies show the promise of being disruptive, but enabling for ORS and very low-cost systems while potentially reducing cost and schedule for a broad range of systems. The introduction of Plug-and-Play (PnP) technologies to facilitate rapid integration may be effective in developing an ADCS that can be developed faster and at lower cost than current, traditional methods allow. However, this rapid integration and reduced non-recurring cost comes with an additional initial non-recurring engineering cost for implementing PnP. The goal is to demonstrate the potential of PnP ADCS by showing the improvements in performance, cost, and schedule, when the PnP ADCS software is demonstrated and tested. Additionally, the implementation of a Direct Model Reference Adaptive Controller (DMRAC) as the core for the ADCS software shows promise as an efficient method of providing stable, accurate control without requiring the extensive analysis, evaluation and gain tailoring that is typically required of more traditional controllers. Microcosm, with partner HRP Systems and graduate student Seth Harvey, have created prototype flight software that facilitates rapid integration through the implementation of PnP concepts while providing control performance suitable for many ORS missions, through the use of adaptive control algorithms. This paper will describe the software architecture, software implementation, adaptive control approach, and early evaluation results that are associated with the sponsor- ed development of this PnP ADCS software.
Keywords
adaptive control; aerospace computing; attitude control; military aircraft; attitude determination; control system; direct model reference adaptive controller; flight software; operationally responsive space; plug-and-play technology; warfighter spacecraft; Adaptive control; Control systems; Costs; Position measurement; Programmable control; Software performance; Software prototyping; Software systems; Software testing; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526507
Filename
4526507
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