NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Importance of Model Simulations in Cassini In-Flight Mission EventsSimulation environments have been an integral part of Cassini's heritage. From the time of flight software development and testing to the beginning of the spacecraft's extended mission operations, both softsim and hardware-in-the-loop testbeds have played vital roles in verifying and validating key mission events. Satellite flybys and mission-critical events have established the need to model Titan's atmospheric torque, Enceladus' plume density, and other key parametric spacecraft environments. This paper will focus on enhancements to Cassini's Flight Software Development System (FSDS) and Integrated Test Laboratory (ITL) to model key event attributes which establish valid test environments and ensure safe spacecraft operability. Comparisons between simulated to in-flight data are presented which substantiate model validity.
Document ID
20150011936
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Brown, Jay
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wang, Eric
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hernandez, Juan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lee, Allan Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
July 1, 2015
Publication Date
August 10, 2009
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference and Exhibit
Location: Chicago, IL
Country: United States
Start Date: August 10, 2009
End Date: August 13, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
FSDS
Enceladus
Titan
hardware-in-the-loop
softsim
ITL

Available Downloads

There are no available downloads for this record.
No Preview Available