Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Henry J. Pernicka"'
Publikováno v:
Journal of Spacecraft and Rockets. 59:360-374
Autor:
Henry J. Pernicka, Jill Davis
Publikováno v:
Acta Astronautica. 155:418-425
Effective space situational awareness/battlespace awareness (SSA/BA) requires determination of resident space object (RSO) characteristics. Responsive SSA can often be enhanced with the use of small inspector satellites due to their relative ease to
Autor:
Henry J. Pernicka, D. Jennings
Publikováno v:
2021 IEEE Aerospace Conference (50100).
The increased interest in satellite formations and deep space exploration drives the need to better understand and explore relative trajectories at the collinear libration points. This paper presents a preliminary study in applying a genetic algorith
Autor:
Henry J. Pernicka, D. Jennings
Publikováno v:
2020 IEEE Aerospace Conference.
The work this paper describes identifies continuous natural relative trajectories near the collinear libration points numerically from the nonlinear CR3BP differential equations by utilizing a shooting method with a two-level differential corrector.
Autor:
Henry J. Pernicka, Jill Davis
Publikováno v:
2020 IEEE Aerospace Conference.
The small satellite revolution has opened the door to a new era in satellite development. As spacecraft hardware continues to advance, traditional monolithic satellites can be replaced with cooperative swarms of smaller spacecraft. To enable an effec
Publikováno v:
2020 IEEE Aerospace Conference.
A key element of the Advanced Propulsion Experiment (APEX) spacecraft mission is the accurate thrust determination of a Multi-Mode Ionic Monopropellant Electrospray (MIME) thruster payload. The MIME thruster payload operates in high thrust, low speci
Autor:
Henry J. Pernicka, Jill Davis
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
Journal of Guidance, Control, and Dynamics. 38:1699-1713
A method for performing bearings-only initial relative orbit determination of a nearby space object in the absence of any information regarding the space object’s geometry and relative orbit is presented. To resolve the range ambiguity characterist
Publikováno v:
Journal of Aerospace Information Systems. 11:679-690
Software design and development often presents a high-risk element during the execution of engineering projects due to the difficulty of identifying defects during late stages of development. Many defects identified during the late stages of small sp
Publikováno v:
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.