Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Robin M. Pinson"'
Autor:
Robin M. Pinson, Ping Lu
Publikováno v:
Journal of Guidance, Control, and Dynamics. 41:1243-1256
Mission proposals that land on asteroids are becoming popular. However, in order to have a successful mission the spacecraft must reliably and softly land at the intended landing site. The problem under investigation is how to design a fuel-optimal p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e287cc748625e3b6ae801414504790ab
https://doi.org/10.2514/1.g003045
https://doi.org/10.2514/1.g003045
Autor:
Robin M. Pinson, John M. Hanson
Publikováno v:
Journal of Spacecraft and Rockets. 49:353-363
This paper addresses different methods for determining the amount of extra propellant (flight performance reserve or FPR) that is necessary to reach orbit with a high probability of success. One approach involves assuming that the various influential
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::697b923662ec1e5963ec3feaadfbdb25
https://doi.org/10.2514/1.a32069
https://doi.org/10.2514/1.a32069
Publikováno v:
Acta Astronautica. 68:571-575
In the early to mid-2000s, NASA made substantial progress in the development of solar sail propulsion systems. Solar sail propulsion uses the solar radiation pressure exerted by the momentum transfer of reflected photons to generate a net force on a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c3e6d6e58f77b817d4f6b9e07474a93
https://doi.org/10.1016/j.actaastro.2010.02.008
https://doi.org/10.1016/j.actaastro.2010.02.008
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
This paper addresses different methods for determining the amount of extra propellant (flight performance reserve or FPR) that is necessary to reach orbit with a high probability of success. One approach involves assuming that the various influential
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf04b37ac91e165f3bfb9c249a19ee15
https://doi.org/10.2514/6.2011-6650
https://doi.org/10.2514/6.2011-6650
Autor:
Jason Hopkins, Timothy Monk, Keithe Baggett, Ian Dux, Jon Holladay, John Jaap, Chad Brown, Robin M. Pinson
Publikováno v:
2011 Aerospace Conference.
The reference heavy-lift launch vehicle (Ares V) for NASA's Constellation Program served as the Point of Departure for Mars Design Reference Architecture 5.0 (DRA 5.0)1, 2. The Ares V vehicle consists of two 5-segment reusable solid rocket boosters,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb14c30bb8a9d21df316692dc4f0dd54
https://doi.org/10.1109/aero.2011.5747484
https://doi.org/10.1109/aero.2011.5747484
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference and Exhibit.
From March to July of 2007, the DARPA Orbital Express mission achieved a number of firsts in autonomous spacecraft operations. The NASA Advanced Video Guidance Sensor (AVGS) was the primary docking sensor during the first two dockings and was used in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45d22923a2e616f7813a29733432b1a6
https://doi.org/10.2514/6.2008-6937
https://doi.org/10.2514/6.2008-6937
Publikováno v:
AIAA Guidance, Navigation and Control Conference and Exhibit.
Orbital Express (OE) was a successful mission demonstrating automated rendezvous and docking. The 2007 mission consisted of two spacecraft, the Autonomous Space Transport Robotic Operations (ASTRO) and the Next Generation Serviceable Satellite (NEXTS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b55a49a1f16c280478526fd87d07692
https://doi.org/10.2514/6.2008-7318
https://doi.org/10.2514/6.2008-7318
Publikováno v:
AIAA Guidance, Navigation and Control Conference and Exhibit.
Six degree-of-freedom (DOF) launch vehicle trajectories are designed to follow an optimized 3-DOF reference trajectory. A vehicle has a finite amount of control power that it can allocate to performing maneuvers. Therefore, the 3-DOF trajectory must
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a14542edbaa7076650aad3df4760b096
https://doi.org/10.2514/6.2008-6292
https://doi.org/10.2514/6.2008-6292
Publikováno v:
2008 IEEE Aerospace Conference.
In May 2007 the first US-sponsored fully autonomous rendezvous and capture was successfully performed by DARPA's Orbital Express (OE) mission. For the following three months, the Boeing ASTRO spacecraft and the Ball Aerospace NEXTSat performed multip
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e5f21526b41c9ef387da49e61721a43
https://doi.org/10.1109/aero.2008.4526518
https://doi.org/10.1109/aero.2008.4526518