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MONTE: the Next Generation of Mission Design and Navigation SoftwareThe Mission Analysis, Operations and Navigation Toolkit Environment (MONTE) is an astrodynamic toolkit produced by the Mission Design and Navigation Software Group at the Jet Propulsion Laboratory. It provides a single integrated environment for all phases of deep space and Earth orbiting missions. Capabilities include: trajectory optimization and analysis, operational orbit determination, flight path control, and 2D/3D visualization. MONTE is presented to the user as an importable Python language module. This allows a simple but powerful user interface via CLUI or script. In addition, the Python interface allows MONTE to be used seamlessly with other canonical scientific programming tools such as SciPy, NumPy, and Matplotlib. MONTE is the prime operational orbit determination software for all JPL navigated missions.
Document ID
20190025536
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Evans, Scott
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Taber, William
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Drain, Theodore
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Smith, Jonathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wu, Hsi-Cheng
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Guevara, Michelle
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sunseri, Richard
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Evans, James
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
June 3, 2019
Publication Date
March 14, 2016
Subject Category
Computer Programming And Software
Astrodynamics
Report/Patent Number
JPL-CL-16-0971
Report Number: JPL-CL-16-0971
Meeting Information
Meeting: International Conference on Astrodynamics Tools and Techniques (ICATT)
Location: Darmstadt
Country: Germany
Start Date: March 14, 2016
End Date: March 17, 2016
Sponsors: European Space Agency
Distribution Limits
Public
Copyright
Other
Keywords
Optimization
Software
Orbit Determination

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