Literatura académica sobre el tema "Automated Rendezvous and Docking"
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Artículos de revistas sobre el tema "Automated Rendezvous and Docking"
Kemble, Stephen. "Automated Rendezvous and Docking of Spacecraft". Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 221, n.º 6 (junio de 2007): 997. http://dx.doi.org/10.1177/095441000722100603.
Texto completoKawano, Isao, Masaaki Mokuno, Hiroshi Koyama y Taichi Nakamura. "Space robot. Guidance and Control for the Automatic Rendezvous Docking Technology. Engineering Test Satellite VII Rendezvous Docking System." Journal of the Robotics Society of Japan 14, n.º 7 (1996): 935–39. http://dx.doi.org/10.7210/jrsj.14.935.
Texto completoHU, Jun, Hao ZHANG, YongChun XIE y HaiXia HU. "Automatic control system design of Shenzhou spacecraft for rendezvous and docking". SCIENTIA SINICA Technologica 44, n.º 1 (1 de enero de 2014): 12–19. http://dx.doi.org/10.1360/092013-1263.
Texto completoZhao, Xia, Quan Gan y Tian Hua Lin. "Multi-Slide-Mode Control for the Homing Phase of Automatic Rendezvous and Docking". Applied Mechanics and Materials 336-338 (julio de 2013): 599–603. http://dx.doi.org/10.4028/www.scientific.net/amm.336-338.599.
Texto completoZhang, Pan y Ma. "Real-Time Docking Ring Detection Based on the Geometrical Shape for an On-Orbit Spacecraft". Sensors 19, n.º 23 (28 de noviembre de 2019): 5243. http://dx.doi.org/10.3390/s19235243.
Texto completoXu, Haojian. "Wigbert Fehse, Automated Rendezvous and Docking of Spacecraft, Cambridge University Press, Cambridge, ISBN: 0-521-82492-3, 2003 (price: $ 120, pp. 495)". Automatica 41, n.º 7 (julio de 2005): 1295–97. http://dx.doi.org/10.1016/j.automatica.2005.02.005.
Texto completoChen, Zhiming, Zhouhuai Luo, Yunhua Wu, Wei Xue y Wenxing Li. "Research on High-Precision Attitude Control of Joint Actuator of Three-Axis Air-Bearing Test Bed". Journal of Control Science and Engineering 2021 (25 de marzo de 2021): 1–11. http://dx.doi.org/10.1155/2021/5582541.
Texto completoHou, Shu Ping, Xiao Yan Wang y Jian Nan Zhang. "A Method of Rendezvous and Docking Based on the 6-DOF Parallel Mechanism in Subsea Environment". Applied Mechanics and Materials 574 (julio de 2014): 651–57. http://dx.doi.org/10.4028/www.scientific.net/amm.574.651.
Texto completoKOYAMA, Hiroshi. "Rendezvous & Docking of Spacecraft". Journal of the Society of Mechanical Engineers 110, n.º 1066 (2007): 704–5. http://dx.doi.org/10.1299/jsmemag.110.1066_704.
Texto completoPairot, J. M., M. Frezet, J. Tailhades, W. Fehse, A. Tobias y A. Getzschmann. "European rendezvous and docking system". Acta Astronautica 28 (agosto de 1992): 31–42. http://dx.doi.org/10.1016/0094-5765(92)90007-6.
Texto completoTesis sobre el tema "Automated Rendezvous and Docking"
Duzzi, Matteo. "Spacecraft Rendezvous and Docking Using Electromagnetic Interactions". Doctoral thesis, Università degli studi di Padova, 2018. http://hdl.handle.net/11577/3422295.
Texto completoLa capacità di eseguire operazioni di servizio su veicoli in orbita ha riscontrato, negli ultimi anni, un’enorme interesse da parte delle maggiori compagnie e agenzie spaziali internazionali. La necessità di ridurre i costi di produzione, assieme alla possibilità di ottenere sistemi complessi più affidabili e duraturi, ha indirizzato marcatamente il mercato dell’ingegneria aerospaziale verso lo studio di soluzioni innovative per eseguire in orbita operazioni quali rifornimento, aggiornamento e manutenzione di sottositemi, riparazioni di componenti non funzionanti e ispezioni. Le nuove idee e tecnologie in via di sviluppo per eseguire queste operazioni sono percepite come estremamente funzionali e efficienti in termini di costo, in grado di estendere la vita operativa di un satellite e diminuire i costi connessi alla sua completa sostituzione. Attualmente, il tassello mancante per poter procedere efficacemente con questo tipo di procedure, è un sistema automatico di docking che possa costituire un nuovo standard semplice ed affidabile. Gli odierni sistemi di docking, infatti, sono caratterizzati da elevati requisiti di puntamento e necessitano dell’attuazione di precise azioni sul controllo d’assetto in modo da garantire un aggancio sicuro tra i due veicoli coinvolti nella manovra. Questo è dovuto al fatto che tali sistemi di aggancio sono stati progettati quasi unicamente per il trasferimento di equipaggio o di materiali mentre nessuna progettazione, finora, è mai stata prevista per i satelliti commerciali e scientifici. Recentemente, l’avvento dei CubeSat ha fortemente incoraggiato aziende e agenzie del settore aerospaziale ad investire nello sviluppo di dimostratori tecnologici e payload scientifici, grazie alla notevole riduzione nel costo necessario per lanciare in orbita tali veicoli. Lo svantaggio nell’utilizzare questo tipo di piattaforme è principalmente legato ai limiti tecnici intrinseci degli stessi, rappresentati dalle ridotte risorse a disposizione. Ciononostante, gran parte di queste limitazioni sono state superate grazie alla possibilità di scalare i risultati ottenuti ed applicarli a sistemi più grandi. Numerose tecnologie sono già state testate e caratterizzate nello spazio usando moduli CubeSat, ma solo esperimenti marginali sono stati condotti sino ad oggi su sistemi di docking, anche se si sta percependo un cambio di tendenza. Tali sistemi, infatti, permetterebbero l’esecuzione di operazioni di aggancio e sgancio, ampliando enormemente i possibili scenari di missione: sistemi modulari formati da molteplici unità CubeSat potrebbero interagire tra loro creando agglomerati più grandi in grado di condividere le risorse più efficacemente, riorganizzarsi e aggiornarsi autonomamente. Lo scopo di questa ricerca è quello di proporre un nuovo sistema di soft-docking caratterizzato da requisiti meno stringenti per quanto concerne l’accuratezza nel puntamento e nel controllo d’assetto rispetto ai sistemi esistenti. L’idea innovativa alla base dello studio è quella di sfruttare la capacità di auto-allineamento e reciproca attrazione garantita dall’interazione magnetica che si instaura tra due interfacce elettromagnetiche, in modo da facilitare le manovre di prossimità ed aggancio. La trattazione è suddivisa in due parti principali. Nella prima parte viene presentato l’esperimento PACMAN (Position and Attitude Control with MAgnetic Navigation) il quale rappresenta un dimostratore tecnologico di un sistema di docking per piccoli satelliti basato su attuatori magnetici. Tale sistema, sviluppato all'interno del programma ESA Education Fly Your Thesis! 2017, è stato testato in gravità ridotta durante la 68th campagna di voli parabolici ESA a dicembre. La seconda parte si focalizza invece su un nuovo concept, TED (Tethered Electromagnetic Docking), secondo il quale le manovre di close-range rendezvous e docking possono essere realizzate lanciando una sonda elettromagnetica collegata ad un filo da un satellite chaser verso un’interfaccia elettromagnetica montata su di un satellite target. Stabilito il collegamento, tramite il recupero del filo, i due veicoli sono connessi rigidamente concludendo la manovra.
MAMMARELLA, MARTINA. "A Comprehensive Modeling Framework for Integrated Mission Analysis and Design of a Reusable Electric Space Tug". Doctoral thesis, Politecnico di Torino, 2019. http://hdl.handle.net/11583/2750013.
Texto completoSeito, Narumi. "Modelagem e simulação de rendezvous e docking". Instituto Nacional de Pesquisas Espaciais (INPE), 2015. http://urlib.net/sid.inpe.br/mtc-m21b/2015/06.03.14.07.
Texto completoIn this thesis strategies to solve the problem of the RVD/B (RendezVous and Docking/Berthing) orbital operations are studied. In a brief review of the literature, the strategies of approximation, the techniques for orbit and attitude synchronization, and the technique for the close proximity approximation are presented, all of them supported by two systems of differential equations for the translational and rotational motion of both spacecrafts. Two configurations are considered for the chaser: one when the robotic manipulator of the chaser is inert, and a second one when the robotic manipulator is in action. In the first configuration the Newtonian formulation is used to obtain the equations of Hill-Clohessy-Klein for the translational dynamics, while the attitude motion is determined by Eulers equations. These two systems of differential equations allow to guide the chaser up to the point for berthing the target. In the second configuration, the Lagrangian formulation for quasi-coordinates and generalized coordinates supplies the equations for the motion of the robotic manipulator when berthing the target. These latter equations and their numerical simulation of berthing the target are the original part of this thesis. The computational simulations of the dynamics are carried out by use of the software MatLab.
Maaroufi, Helmi. "Dynamics and Control of Unmanned Spacecraft Rendezvous and Docking". Thesis, KTH, Farkost och flyg, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-209188.
Texto completoI denna rapport utreds olika faser avrymdfarkosters rendezvous och docknings manövrar (RvD) samtundersöks en rad matematiska modeller för formationsflygning,nämligen de icke-linjära ekvationerna av relativ rörelse (NERM)och Hill-Clohessy-Wiltshire-ekvationer (HCW). Dessa dynamiskasystemmodeller beskriver formationsflygningen i både ostörd ochstörd omgivning. Vidare undersöks alternativa reglermetoder ochen filtreringsmetod såsom Linjär Kvadratisk Regulator (LQR),Linjär Kvadratisk Gaussisk (LQG) och utökad Kalman filtrering(EKF), för att reducera både tid och ΔV-kostnaden för hela rymduppdraget.Målen med dessa reglermetoder är att rymdfarkostensjälvständigt skall kunna utföra rendezvous och dockning.
Andersson, Oscar y Lucas Molin. "AutoTruck : Automated docking with internal sensors". Thesis, KTH, Maskinkonstruktion (Inst.), 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-230383.
Texto completoKandidatarbetet syftar till att undersöka hur ett ledatfordon kan parkera sig självt efter en förbestämd parkeringsruttmed en kombination av flera ultraljudssensorersamt en vinkelgivare.Projektet består av två delar; konstruktion av ett miniatyrfordonsamt mjukvaran som styr fordonet. Fordonettillverkades från butiksköpta komponenter och skräddarsyddadelar. Lastbilens design var baserad p°a en bakhjulsdrivenAckermannstyrd lastbil. Identifieringen av en parkeringsplatssamt avståndsmätning hanterades av ultraljudssensoreroch hitch vinkeln mättes av en vinkelgivare.Miniatyrfordonets prestanda utvärderades genom attmäta släpets vinkelskillnad från centerlinjen av parkeringsplatsen.Prestandan ansågs att vara tillräckligt god med lyckadeparkeringar i 8 av 10 tester.
ANDERSSON, OSCAR y LUCAS MOLIN. "AutoTruck : Automated docking with internal sensors". Thesis, KTH, Mekatronik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-233142.
Texto completoKandidatarbetet syftar till att undersöka hur ett ledat fordon kan parkera sig självt efter en förbestämd parkeringsrutt med en kombination av flera ultraljudssensorer samt en vinkelgivare. Projektet består av två delar; konstruktion av ett miniatyrfordon samt mjukvaran som styr fordonet. Fordonet tillverkades från butiksköpta komponenter och skräddarsydda delar. Lastbilens design var baserad på en bakhjulsdriven Ackermannstyrd lastbil. Identifieringen av en parkeringsplats samt avståndsmätning hanterades av ultraljudssensorer och hitch vinkeln mättes av en vinkelgivare. Miniatyrfordonets prestanda utvärderades genom att mäta släpets vinkelskillnad från centerlinjen av parkeringsplatsen. Prestandan ansågs att vara tillräckligt god med lyckade parkeringar i 8 av 10 tester.
Simpson, Richard Edward. "Engineering a coordinated rendezvous system for docking USVs to ships using GPS positioning". Thesis, University of Bristol, 2015. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.707706.
Texto completoHettrick, Hailee Elida. "Autonomous rendezvous and docking with tumbling, uncooperative, and fragile targets under uncertain knowledge". Thesis, Massachusetts Institute of Technology, 2019.
Buscar texto completoThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2019
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 189-194).
As efforts to expand humanity's presence in space continue to increase, a need for spacecraft to autonomously perform in-space close proximity maneuvers without a human operator increases, as well. Such in-space close proximity maneuvers include active debris removal, satellite servicing, and in-space assembly. Active debris removal will facilitate the continued use and access to low Earth orbit, mitigating the exponential debris growth occurring due to decrepit satellites and rocket bodies colliding. Satellite servicing will provide the capability to repair and refurbish spacecraft, elongating the lifetime of valuable assets both locally orbiting Earth and on routes further out in the solar system. In-space assembly is the means by which large space structures are developed in orbit. Currently, such feats occur with the help of astronauts and robotic arms (i.e. the continued development of the International Space Station). However, for increased benefit, in-space assembly must occur autonomously, without a human in-the-loop, in order to create large structures in locations unideal for humans or with a non-negligible communication latency. These three reference missions need the software enabling autonomous rendezvous and docking to reach a technical readiness level to be employed with confidence. In-space close proximity maneuvers share a standard sequence of events described in this thesis. The focus of this thesis address the terminal approach trajectory to soft docking, the contact dynamics of docking between two spacecraft, the optimization of the detumble procedure to bring the Target to stabilization, and adaptive control techniques to handle uncertainties in spacecraft knowledge. The software developed in support of these subproblems is included in the appendices and is largely based on implementation with the Synchronized Position Hold Engage Reorient Experimental Satellites (SPHERES) platform or with the characteristics of SPHERES considered.
by Hailee Elida Hettrick.
S.M.
S.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronautics
Jewison, Christopher Michael. "Guidance and control for multi-stage rendezvous and docking operations in the presence of uncertainty". Thesis, Massachusetts Institute of Technology, 2017. http://hdl.handle.net/1721.1/112362.
Texto completoThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references (pages 251-267).
Rendezvous and docking missions have been a mainstay of space exploration from the Apollo program through present day operations with the International Space Station. There remains a growing interest in several mission types that not only rely on rendezvous and docking, but also rely on maneuvering spacecraft once docked. For example, there is active interest in orbital debris removal, on-orbit assembly, on-orbit refueling, and on-orbit servicing and repair missions. As these missions become more and more popular, the number of rendezvous and docking class operations will increase dramatically. Current methods focus on performing rendezvous and docking to very well-known targets and in very well-known conditions. Inherent to these new mission types, however, is an increasing element of uncertainty to which new guidance and control architectures will need to be robust. As guidance and control techniques become more robust, a corresponding tradeoff in performance can typically be experienced. This thesis attempts to address the uncertainties in rendezvous and docking operations while maintaining a probabilistically optimal level of performance. There are two main focuses in the thesis: spacecraft trajectory optimization and reference-tracking controller selection. With respect to trajectory optimization, the goal is to nd probabilistically optimal trajectories given large uncertainties in mission critical parameters, such as knowledge of an obstacle's position, while knowing that the trajectory is able to be replanned onboard the spacecraft when higher precision information is obtained. This baseline optimal trajectory and subsequently replanned trajectories are then followed by an optimally determined set of reference-tracking controllers. These controllers are selected and scheduled throughout the phases of the mission based on the probabilistically expected performance in the presence of noise and uncertain parameters. This process is explored through its implementation on a generic problem setup for rendezvous, docking, and joint maneuvering. Results specfic to this problem and associated analysis motivate the use of probabilistic planning in future space missions. Specically, the thesis shows that fuel and tracking performance can be improved if multi-stage missions are planned continuously through phase transitions and without the use of waypoints. Furthermore, under the presence of large uncertainties, the techniques in this thesis produce better expected fuel and tracking performance than traditional trajectory planning and controller selection methods.
by Christopher Michael Jewison.
Ph. D.
Scheithauer, Amy T. "3D Relative Position and Orientation Estimation for Rendezvous and Docking Applications Using a 3D Imager". Ohio University / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1265809623.
Texto completoLibros sobre el tema "Automated Rendezvous and Docking"
H, Tolson Robert y Langley Research Center, eds. Evaluation of GPS position and attitude determination for automated rendezvous and docking missions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoHang tian qi zi dong jiao hui dui jie: Automated rendezvous and docking of spacecraft. Beijing: Zhongguo yu hang chu ban she, 2013.
Buscar texto completoKong jian jiao hui dui jie ce liang ji shu ji gong cheng ying yong. Beijing Shi: Zhongguo yu hang chu ban she, 2005.
Buscar texto completoSyromi︠a︡tnikov, V. S. 100 stories about docking and other adventures in space and on Earth. Moscow: Universitetskaya kniga, 2005.
Buscar texto completoJiao hui dui jie: Rendezvous and docking. Beijing Shi: Guo fang gong ye chu ban she, 2012.
Buscar texto completoSyromi͡atnikov, V. S. Spacecraft docking devices. Princeton, N.J. (P.O. Box 82, Princeton 08542): Space Studies Institute, 1990.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Automated rendezvous and capture demonstration study: Final report. Huntsville, Ala: Applied Research Inc., 1993.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Automated rendezvous and capture demonstration study: Final report. Huntsville, Ala: Applied Research Inc., 1993.
Buscar texto completoHaines, Richard F. Space vehicle approach velocity judgments under simulated visual space conditions. Moffett Field, Calif: Ames Research Center, 1987.
Buscar texto completoXie, Yongchun, Changqing Chen, Tao Liu y Min Wang. Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6990-6.
Texto completoCapítulos de libros sobre el tema "Automated Rendezvous and Docking"
Wang, Zhenhua, Zhaohui Chen, Guofeng Zhang y Hanxiao Zhang. "Automatic Test of Space Rendezvous and Docking GNC Software". En Lecture Notes in Electrical Engineering, 81–92. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-34531-9_9.
Texto completoXie, Yongchun, Changqing Chen, Tao Liu y Min Wang. "Automatic Control Method and Scheme Design for Rendezvous and Docking". En Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods, 219–80. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6990-6_5.
Texto completoWoods, W. David. "Rendezvous and docking". En How Apollo Flew to the Moon, 395–428. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-7179-1_13.
Texto completoYang, Yaguang. "Spacecraft Rendezvous and Docking". En Spacecraft Modeling, Attitude Determination, and Control Quaternion-based Approach, 249–66. Boca Raton, FL : CRC Press, 2019. | “A science publishers book.”: CRC Press, 2019. http://dx.doi.org/10.1201/9780429446580-15.
Texto completoYang, Hong. "Manned Rendezvous and Docking Technology". En Manned Spacecraft Technologies, 185–96. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-4898-7_6.
Texto completoXie, Yongchun, Changqing Chen, Tao Liu y Min Wang. "Simulation Verification of Rendezvous and Docking". En Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods, 449–77. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6990-6_9.
Texto completoXie, Yongchun, Changqing Chen, Tao Liu y Min Wang. "Rendezvous Kinematics and Dynamics". En Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods, 37–66. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-6990-6_2.
Texto completoLi, Dongyu, Shuzhi Sam Ge y Tong Heng Lee. "Time-Synchronized Spacecraft Control in Rendezvous and Docking". En Time-Synchronized Control: Analysis and Design, 189–220. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-3089-7_8.
Texto completoWang, Baozhi. "Modeling and Simulation in Rendezvous and Docking Spaceflight Training". En Proceedings of the 14th International Conference on Man-Machine-Environment System Engineering, 399–407. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-662-44067-4_48.
Texto completoLi, Bin, Zuo Xun Li y Kai Zhang. "Distributionally Model Predictive Control for Spacecraft Rendezvous and Docking". En Lecture Notes in Electrical Engineering, 4447–57. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8155-7_369.
Texto completoActas de conferencias sobre el tema "Automated Rendezvous and Docking"
Williamson, Marlin, Nick Johnston, Richard T. Howard, Drew P. Hall, Joseph Gaines y Katherine Chavis. "Automated rendezvous and docking operations evaluations". En Defense and Security Symposium, editado por Pejmun Motaghedi. SPIE, 2006. http://dx.doi.org/10.1117/12.668352.
Texto completoGuglieri, Giorgio, Fulvia Quagliotti, Antonio Saluzzi y Pasquale Pellegrino. "Analysis of Automated Rendezvous and Docking Operations". En AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-6766.
Texto completoHoward, Richard T., Connie K. Carrington y Mohamed S. El-Genk. "Multi-Sensor Testing for Automated Rendezvous and Docking". En 008. AIP, 2008. http://dx.doi.org/10.1063/1.2845037.
Texto completoZhu, Xiang. "Optical design of space cameras for automated rendezvous and docking systems". En Sensors and Systems for Space Applications XI, editado por Khanh D. Pham y Genshe Chen. SPIE, 2018. http://dx.doi.org/10.1117/12.2305238.
Texto completoMitchell, Jennifer D., Scott P. Cryan, David Strack, Linda L. Brewster, Marlin J. Williamson, Richard T. Howard y A. S. Johnston. "Automated Rendezvous and Docking Sensor Testing at the Flight Robotics Laboratory". En 2007 IEEE Aerospace Conference. IEEE, 2007. http://dx.doi.org/10.1109/aero.2007.352723.
Texto completoHoward, Richard T., Marlin L. Williamson, Albert S. Johnston, Linda L. Brewster, Jennifer D. Mitchell, Scott P. Cryan, David Strack y Kevin Key. "Automated rendezvous and docking sensor testing at the flight robotics laboratory". En Defense and Security Symposium, editado por Richard T. Howard y Robert D. Richards. SPIE, 2007. http://dx.doi.org/10.1117/12.723437.
Texto completoTOBIAS, A., W. FEHSE, D. WILDE, J. PAIROT y F. PAOLI. "Intervention of human operators in automated spacecraft Rendezvous and Docking GNC". En Navigation and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2791.
Texto completoTurbe, Michael, James McDuffie, Brandon DeKock, Kevin Betts y Connie Carrington. "SPARTAN: A High-Fidelity Simulation for Automated Rendezvous and Docking Applications". En AIAA Modeling and Simulation Technologies Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-6806.
Texto completoHannah, S. Joel. "A relative navigation application of ULTOR technology for automated rendezvous and docking". En Defense and Security Symposium, editado por Richard T. Howard y Robert D. Richards. SPIE, 2006. http://dx.doi.org/10.1117/12.665055.
Texto completoHoward, Richard T., Thomas C. Bryan, Michael L. Book y John L. Jackson. "Active sensor system for automatic rendezvous and docking". En AeroSense '97, editado por Gary W. Kamerman. SPIE, 1997. http://dx.doi.org/10.1117/12.281001.
Texto completoInformes sobre el tema "Automated Rendezvous and Docking"
Smith, Samuel M. y Stanley E. Dunn. Enhancing AUV Operational Capabilities: Hovering, Rendezvous, and Docking. Fort Belvoir, VA: Defense Technical Information Center, septiembre de 1997. http://dx.doi.org/10.21236/ada628288.
Texto completoJatko, W. B., J. S. Goddard, R. K. Ferrell, S. S. Gleason, J. S. Hicks y V. K. Varma. Crusader Automated Docking System Phase 3 report. Office of Scientific and Technical Information (OSTI), marzo de 1996. http://dx.doi.org/10.2172/230272.
Texto completoKring, C. T., V. K. Varma y W. B. Jatko. Crusader Automated Docking System: Technology support for the Crusader Resupply Team. Interim report, Ammunition Logistics Program. Office of Scientific and Technical Information (OSTI), noviembre de 1995. http://dx.doi.org/10.2172/208313.
Texto completoDrotning, W. D. Automated waste canister docking and emplacement using a sensor-based intelligent controller; Yucca Mountain Site Characterization Project. Office of Scientific and Technical Information (OSTI), agosto de 1992. http://dx.doi.org/10.2172/140803.
Texto completo