Fuel-optimal control for soft landing on an irregular asteroid
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[1] Hexi Baoyin,et al. Generating families of 3D periodic orbits about asteroids , 2012 .
[2] Dante S. Lauretta,et al. An Overview of the OSIRIS-REx Asteroid Sample Return Mission , 2012 .
[3] J. Veverka,et al. Implementation of the first asteroid landing , 2002 .
[4] M. Zolensky,et al. MarcoPolo-R near earth asteroid sample return mission , 2011 .
[5] D. Scheeres,et al. Exterior gravitation of a polyhedron derived and compared with harmonic and mascon gravitation representations of asteroid 4769 Castalia , 1996 .
[6] Daniel J. Scheeres,et al. Preliminary Planning for NEAR's Low-Altitude Operations at 433 Eros , 1999 .
[7] R. Epenoy,et al. New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation , 2002 .
[8] Jesús Gil-Fernández,et al. Practical Method for Optimization of Low-Thrust Transfers , 2010 .
[9] G. Rauwolf,et al. Near-optimal low-thrust orbit transfers generated by a genetic algorithm , 1996 .
[10] Y. Tsuda,et al. System design of the Hayabusa 2—Asteroid sample return mission to 1999 JU3 , 2013 .
[11] Daniel J. Scheeres,et al. Finite-time control for spacecraft body-fixed hovering over an asteroid , 2015, IEEE Transactions on Aerospace and Electronic Systems.
[12] K. Teo,et al. THE CONTROL PARAMETERIZATION METHOD FOR NONLINEAR OPTIMAL CONTROL: A SURVEY , 2013 .
[13] Hexi Baoyin,et al. Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach , 2012 .
[14] Cui Pingyuan,et al. An autonomous optical navigation and guidance for soft landing on asteroids , 2004 .
[15] M. Guelman,et al. Power limited soft landing on an asteroid , 1994 .
[16] Daniel J. Scheeres,et al. CONTROL OF HOVERING SPACECRAFT USING ALTIMETRY , 2000 .
[17] Lorenzo Casalino,et al. Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions , 1998 .
[18] Masashi Uo,et al. Hayabusa-final autonomous descent and landing based on target marker tracking , 2006 .
[19] G. Lantoine,et al. Optimal trajectories for soft landing on asteroids AE 8900 , 2006 .
[20] Junfeng Li,et al. Earth-crossing asteroid intercept mission with a solar sail spacecraft , 2014, IEEE Aerospace and Electronic Systems Magazine.
[21] J. Miller,et al. Evaluation of the Dynamic Environment of an Asteroid: Applications to 433 Eros , 2000 .
[22] Jorge J. Moré,et al. User Guide for Minpack-1 , 1980 .
[23] J. Miller,et al. Determination of Shape, Gravity, and Rotational State of Asteroid 433 Eros , 2002 .
[24] I. Michael Ross,et al. Direct trajectory optimization by a Chebyshev pseudospectral method , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).
[25] Yanning Guo,et al. ZEM/ZEV Feedback Guidance Application to Fuel-Efficient Orbital Maneuvers Around an Irregular-Shaped Asteroid , 2012 .
[26] Junfeng Li,et al. Pseudospectral Methods for Trajectory Optimization with Interior Point Constraints: Verification and Applications , 2013, IEEE Transactions on Aerospace and Electronic Systems.
[27] Derek F Lawden,et al. Optimal trajectories for space navigation , 1964 .