Libration and transverse dynamic stability control of flexible bare electrodynamic tether systems in satellite deorbit

[1]  Franz Newland,et al.  Libration Control of Bare Electrodynamic Tethers Considering Elastic–Thermal–Electrical Coupling , 2016 .

[2]  Nickolas J. Sabey,et al.  General Perturbations Guidance Scheme for Electrodynamic Orbital Maneuvers with Libration Effects , 2016 .

[3]  S. Khan,et al.  Optimum sizing of bare-tape tethers for de-orbiting satellites at end of mission , 2015 .

[4]  Zheng H. Zhu,et al.  Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration , 2015 .

[5]  G. Sánchez-Arriaga,et al.  Impact of Nonideal Effects on Bare Electrodynamic Tether Performance , 2015 .

[6]  C. McInnes,et al.  Concept-of-operations disposal analysis of spacecraft by gossamer structure , 2014, 1410.6727.

[7]  Zheng H. Zhu,et al.  Long-Term Libration Dynamics and Stability Analysis of Electrodynamic Tethers in Spacecraft Deorbit , 2014 .

[8]  R. Mantellato,et al.  Two-bar model for free vibrations damping of space tethers by means of spring-dashpot devices , 2014 .

[9]  Zheng Hong Zhu,et al.  Optimal Control of Nanosatellite Fast Deorbit Using Electrodynamic Tether , 2014 .

[10]  Víctor Lanchares,et al.  Attitude stabilization of electrodynamic tethers in elliptic orbits by time-delay feedback control , 2014 .

[11]  Zheng H. Zhu,et al.  Libration dynamics and stability of electrodynamic tethers in satellite deorbit , 2013 .

[12]  Zheng H. Zhu,et al.  Dynamics of Nanosatellite Deorbit by Bare Electrodynamic Tether in Low Earth Orbit , 2013 .

[13]  Juan R. Sanmartin,et al.  Survival probability of round and tape tethers against debris impact , 2013 .

[14]  A. S. Torres,et al.  Orbital debris mitigation through deorbiting with passive electrodynamic drag , 2012 .

[15]  Franz Newland,et al.  AIM Microsatellite Platform: A Canadian Multi-Mission Satellite Bus Solution , 2012 .

[16]  K. Uldall Kristiansen,et al.  Numerical modelling of elastic space tethers , 2012 .

[17]  Lee-Anne McKinnell,et al.  The international reference ionosphere today and in the future , 2011 .

[18]  Zheng H. Zhu,et al.  Dynamic modeling of cable towed body using nodal position finite element method , 2011 .

[19]  M. Spittel,et al.  Thermal expansion of light metal alloys , 2011 .

[20]  Rui Zhong,et al.  Deorbiting Dynamics of Electrodynamic Tether , 2011 .

[21]  A. Chulliat,et al.  International Geomagnetic Reference Field: the eleventh generation , 2010 .

[22]  Dongping Jin,et al.  Deployment and retrieval of tethered satellite system under J2 perturbation and heating effect , 2010 .

[23]  Hirohisa Kojima,et al.  Stability analysis of in-plane and out-of-plane periodic motions of electrodynamic tether system in inclined elliptic orbit , 2009 .

[24]  Robert Scott,et al.  Deorbiting of Low Earth Orbit (LEO) microsatellites , 2009 .

[25]  Paul Williams,et al.  Libration Control of Electrodynamic Tethers Using Predictive Control with Time-Delayed Feedback , 2009 .

[26]  Keith R. P. Fuhrhop,et al.  Theory and Experimental Evaluation of Electrodynamic Tether Systems and Related Technologies. , 2007 .

[27]  P. Krisko,et al.  Benefits and risks of using electrodynamic tethers to de-orbit spacecraft , 2006 .

[28]  Noboru Takeichi,et al.  Practical Operation Strategy for Deorbit of an Electrodynamic Tethered System , 2006 .

[29]  Jesus Pelaez,et al.  Generator Regime of Self-Balanced Electrodynamic Bare Tethers , 2006 .

[30]  Luciano Iess,et al.  Small Mission Design for Testing In-Orbit an Electrodynamic Tether Deorbiting System , 2006 .

[31]  Satomi Kawamoto,et al.  Precise numerical simulations of electrodynamic tethers for an active debris removal system , 2006 .

[32]  Zheng H. Zhu,et al.  Elastodynamic Analysis of Aerial Refueling Hose Using Curved Beam Element , 2006 .

[33]  N. Johnson,et al.  Risks in Space from Orbiting Debris , 2006, Science.

[34]  Paul Williams,et al.  Energy Rate Feedback for Libration Control of Electrodynamic Tethers , 2006 .

[35]  Vinod J. Modi,et al.  Effect of electrodynamic forces on the orbital dynamics of tethered satellites , 2005 .

[36]  Luciano Iess,et al.  Linear Stability Analysis of Electrodynamic Tethers , 2005 .

[37]  Yoshiki Yamaigiwa,et al.  Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force , 2005 .

[38]  D. Schmidt,et al.  A Preliminary Gravitational Model to Degree 2160 , 2005 .

[39]  Haskan San,et al.  Orbital Maneuvering with Electrodynamic Tethers , 2003 .

[40]  Hironori A. Fujii,et al.  Libration Control of Flexible Tethers Using Electromagnetic Forces and Movable Attachment , 2003 .

[41]  Chris Blanksby,et al.  Heating and modeling effects in tethered aerocapture missions , 2003 .

[42]  D. Drob,et al.  Nrlmsise-00 Empirical Model of the Atmosphere: Statistical Comparisons and Scientific Issues , 2002 .

[43]  Luciano Iess,et al.  Stability and control of electrodynamic tethers for de-orbiting applications , 2001 .

[44]  Mario L. Cosmo,et al.  Two-Bar Model for the Dynamics and Stability of Electrodynamic Tethers , 2002 .

[45]  E. C. Lorenzini,et al.  A New Kind of Dynamic Instability in Electrodynamic Tethers , 2000 .

[46]  R. D. Estes,et al.  The orbital-motion-limited regime of cylindrical Langmuir probes , 1999 .

[47]  Mario L. Cosmo,et al.  Dynamical, Electrical, and Thermal Coupling in a New Class of Electrodynamic Tethered Satellites , 1999 .