Balancing Autonomous Spacecraft Activity Control with an Integrated Scheduler-Planner and Reactive Executive

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$122,776.00
Award Year:
2013
Program:
SBIR
Phase:
Phase I
Contract:
NNX13CA26P
Award Id:
n/a
Agency Tracking Number:
125202
Solicitation Year:
2012
Solicitation Topic Code:
H6.01
Solicitation Number:
n/a
Small Business Information
CO, Denver, CO, 80210-2562
Hubzone Owned:
Y
Minority Owned:
N
Woman Owned:
N
Duns:
806586835
Principal Investigator:
Robert Radicevich
Principal Software Engineer
(303) 864-0556
Bob@redcanyonengineering.com
Business Contact:
Kristin Thomas
Business Official
(303) 864-0556
kristin.thomas@redcanyonsoftware.com
Research Institution:
Stub




Abstract
Spacecraft operations demand a high level of responsiveness in dynamic environments. During operations, it is possible for unexpected events and anomalies to disrupt the mission schedule, and in the case of critical faults, even threaten the health and safety of the spacecraft. Historically, it has been the responsibility of the mission operations team on the ground to issue command sequences and monitor spacecraft health and status to ensure that long-term science, engineering, and safety goals are achieved. Red Canyon Software is building upon previous designs for on-board, layered autonomous software flight systems employing continuous planning and command sequencing. The proposed innovation increases the robustness of on-board autonomy for space vehicle operation, while at the same time offers reductions in mission development costs by leveraging off of newer flight proven software technologies. Also, developing, verifying, and validating spacecraft activity and constraint models for use with model-based autonomous planners and reactive sequencers are difficult and complex activities. For robust, on-board autonomous systems with multiple layers of software performing varying levels of constraint checking prior to activity planning and command sequencing, more than one layer will need to be configured with the same model constraints. To reduce the cost and risk of model development and use, a single, shared spacecraft domain model representation is proposed, along with development of a graphical editor that allows system engineers to easily encode domain information and that uses verification rules to detect inconsistencies or errors.

* information listed above is at the time of submission.

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