The Super Strypi Navigation, Guidance & Control Software is a real-time implementation of the navigation, guidance and control algorithms designed to deliver a payload to a desired orbit for the rail launched Super Strypi launch vehicle. The software contains all flight control algorithms required from pre-launch until orbital insertion. The flight sequencer module calls the NG&C functions at the appropriate times of flight. Additional functionality includes all the low level drivers and I/O for communicating to other systems within the launch vehicle and to the ground support equipment. The software is designed such that changes to the launch location and desired orbit can be changed without recompiling the code.
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Anderson, Mark A., Bigelow, Matthew, Gilkey, Jeff C., Hutchinson, Lance V., Madsen, Jared D., Meindl, Mark A., Outka, David E., and Schrempp, Mark T. Super Strypi Navigation, Guidance & Control (NGC) v. Release 04.
Computer software. Vers. 00. USDOE. 27 May. 2016.
Web.
Anderson, Mark A., Bigelow, Matthew, Gilkey, Jeff C., Hutchinson, Lance V., Madsen, Jared D., Meindl, Mark A., Outka, David E., & Schrempp, Mark T. (2016, May 27). Super Strypi Navigation, Guidance & Control (NGC) v. Release 04 (Version 00) [Computer software].
Anderson, Mark A., Bigelow, Matthew, Gilkey, Jeff C., Hutchinson, Lance V., Madsen, Jared D., Meindl, Mark A., Outka, David E., and Schrempp, Mark T. Super Strypi Navigation, Guidance & Control (NGC) v. Release 04.
Computer software. Version 00. May 27, 2016.
@misc{osti_1331974,
title = {Super Strypi Navigation, Guidance & Control (NGC) v. Release 04, Version 00},
author = {Anderson, Mark A. and Bigelow, Matthew and Gilkey, Jeff C. and Hutchinson, Lance V. and Madsen, Jared D. and Meindl, Mark A. and Outka, David E. and Schrempp, Mark T.},
abstractNote = {The Super Strypi Navigation, Guidance & Control Software is a real-time implementation of the navigation, guidance and control algorithms designed to deliver a payload to a desired orbit for the rail launched Super Strypi launch vehicle. The software contains all flight control algorithms required from pre-launch until orbital insertion. The flight sequencer module calls the NG&C functions at the appropriate times of flight. Additional functionality includes all the low level drivers and I/O for communicating to other systems within the launch vehicle and to the ground support equipment. The software is designed such that changes to the launch location and desired orbit can be changed without recompiling the code.},
doi = {},
url = {https://www.osti.gov/biblio/1331974},
year = {Fri May 27 00:00:00 EDT 2016},
month = {Fri May 27 00:00:00 EDT 2016},
note =
}
