Variable stiffness design for the soft landing of a 2016HO3 asteroid probe

Author:

Ding Jianzhong,Zhou Shiming,Yu Haoran,Wang Chunjie

Funder

Joint Fund for Aerospace Advanced Manufacturing Technology Research

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference45 articles.

1. Modified granular impact force laws for the OSIRIS-REx touchdown on the surface of asteroid (101955) Bennu;Ballouz;Mon. Not. R. Astron. Soc.,2021

2. Variable stiffness composite laminated beams-nonlinear free flexural vibration behavior using a sinusoidal based shear flexible structural theory accounting for Poisson’s effect;Barathan;Int. J. Non-Linear Mech.,2022

3. OSIRIS-REx Touch-And-Go (TAG) mission design and analysis;Berry;Adv. Astronaut. Sci.,2013

4. The philae lander mission and science overview;Boehnhardt;Philos. Trans. Roy. Soc. A: Math., Phys. Eng. Sci.,2017

5. Linear implicit differentiation formulas of variable step and order;van Bokhoven;IEEE Trans. Circ. Syst.,1975

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