Close proximity dynamics and control about asteroids
暂无分享,去创建一个
[1] D. Scheeres,et al. The Effect of C22 on Orbit Energy and Angular Momentum , 1999 .
[2] Akira Fujiwara,et al. Astrodynamics Science about Itokawa, Gravity and Ephemeris , 2006 .
[3] Morad Nazari,et al. Observer-based body-frame hovering control over a tumbling asteroid , 2014 .
[4] D. Scheeres. Dynamics about Uniformly Rotating Triaxial Ellipsoids: Applications to Asteroids , 1994 .
[5] Daniel J. Scheeres,et al. Changes in Rotational Angular Momentum due to Gravitational Interactions between Two Finite Bodies* , 2001 .
[6] Takahide Mizuno,et al. Mass and Local Topography Measurements of Itokawa by Hayabusa , 2006, Science.
[7] Daniel J. Scheeres,et al. The Effect of C 22 on Orbit Energy and Angular Momentum , 1999 .
[8] D. Scheeres,et al. Boundedness of Spacecraft Hovering Under Dead-Band Control in Time-Invariant Systems , 2007 .
[9] D. Scheeres. Orbital motion in strongly perturbed environments , 2012 .
[10] Harry Dankowicz,et al. Some special orbits in the two-body problem with radiation pressure , 1994 .
[11] Daniel J. Scheeres,et al. Stability of Sun-Synchronous Orbits in the Vicinity of a Comet , 2009 .
[12] Daniel J. Scheeres,et al. CONTROL OF HOVERING SPACECRAFT USING ALTIMETRY , 2000 .
[13] D. Scheeres,et al. Exterior gravitation of a polyhedron derived and compared with harmonic and mascon gravitation representations of asteroid 4769 Castalia , 1996 .
[14] Daniel J. Scheeres,et al. Stability bounds for three-dimensional motion close to asteroids , 2002 .
[15] Amit K. Sanyal,et al. Guidance and Control for Spacecraft Autonomous Chasing and Close Proximity Maneuvers , 2012, ROCOND.
[16] Daniel J. Scheeres,et al. Restricted Full Three-Body Problem : Application to Binary System 1999 KW4 , 2008 .
[17] Daniel J. Scheeres,et al. Surface Gravity Fields for Asteroids and Comets , 2013 .
[18] Daniel J. Scheeres,et al. The Actual Dynamical Environment About Itokawa , 2006 .
[19] Daniel J. Scheeres,et al. Small-Body Postrendezvous Characterization via Slow Hyperbolic Flybys , 2011 .
[20] Steven J. Ostro,et al. Shape and Non-Principal Axis Spin State of Asteroid 4179 Toutatis , 1995, Science.
[21] H. U. Keller,et al. On the stability of dust particle orbits around cometary nuclei , 1995 .
[22] J. Miller,et al. Evaluation of the Dynamic Environment of an Asteroid: Applications to 433 Eros , 2000 .
[23] Daniel J. Scheeres,et al. Radar observations and a physical model of Asteroid 1580 Betulia , 2007 .
[24] Masashi Uo,et al. Optical Hybrid Navigation and Station Keeping around Itokawa , 2006 .
[25] D. Scheeres. Orbital mechanics about small bodies , 2012 .
[26] Nathan C. Shupe. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object , 2010 .
[27] D. Scheeres. Orbital motion in strongly perturbed environments : applications to asteroid, comet and planetary satellite orbiters , 2012 .
[28] Daniel J. Scheeres,et al. Satellite Dynamics about Asteroids , 1994 .
[29] Daniel J. Scheeres,et al. A nonlinear observer design for a rigid body in the proximity of a spherical asteroid , 2013 .
[30] Junichiro Kawaguchi,et al. Hayabusa, Detailed Guidance and Navigation Operations during Descents and Touchdowns , 2006 .
[31] F. Mignard,et al. About an unsuspected integrable problem , 1984 .
[32] Daniel J. Scheeres,et al. Spacecraft dynamics in the vicinity of a comet , 2008 .
[33] Daniel J. Scheeres,et al. Spacecraft dynamics far from a comet , 2002 .
[34] Daniel J. Scheeres,et al. Spacecraft hovering control for body-fixed hovering over a uniformly rotating asteroid using geometric mechanics , 2014 .
[35] D. Scheeres,et al. New Solar Radiation Pressure Force Model for Navigation , 2010 .
[36] Daniel J. Scheeres,et al. The Restricted Hill Full 4-Body Problem: application to spacecraft motion about binary asteroids , 2005 .
[37] D. Scheeres,et al. Control of Hovering Spacecraft Near Small Bodies: Application to Asteroid 25143 Itokawa , 2005 .
[38] Daniel J. Scheeres,et al. Satellite Dynamics about Small Bodies: Averaged Solar Radiation Pressure Effects , 1999 .