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    Article

    Sensitivity analysis for a type of statically stable sailcrafts

    Two types of sensitivities are proposed for statically stable sailcrafts. One type is the sensitivities of solar-radiation-pressure force with respect to position of the center of mass, and the other type is t...

    Zheng-Xue Li, Jun-Feng Li, He-** Baoyin in Acta Mechanica Sinica (2012)

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    The experimental study on the contact process of passive walking

    The passive dynamic walking is a new concept of biped walking. Researchers have been working on this area with both theoretical analysis and experimental analysis ever since McGeer. This paper presents our com...

    Feng Qi, Lai-Ye Bi, Tian-Shu Wang, Jun-Feng Li in Acta Mechanica Sinica (2012)

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    A method for classifying orbits near asteroids

    A method for classifying orbits near asteroids under a polyhedral gravitational field is presented, and may serve as a valuable reference for spacecraft orbit design for asteroid exploration. The orbital dynam...

    **an-Yu Wang, Sheng-** Gong, Jun-Feng Li in Acta Mechanica Sinica (2014)

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    A survey on orbital dynamics and navigation of asteroid missions

    Asteroid exploration is currently one of the most concerned topics among international space agencies. Orbital dynamics and navigation are obviously crucial for asteroid exploration. This paper aims to give a ...

    He-** Baoyin, Jun-Feng Li in Acta Mechanica Sinica (2014)

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    Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails

    The advantage of solar sails in deep space exploration is that no fuel consumption is required. The heliocentric distance is one factor influencing the solar radiation pressure force exerted on solar sails. In...

    **g He, Sheng-** Gong, Fang-Hua Jiang, Jun-Feng Li in Acta Mechanica Sinica (2014)

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    Low-thrust trajectory optimization in a full ephemeris model

    The low-thrust trajectory optimization with complicated constraints must be considered in practical engineering. In most literature, this problem is simplified into a two-body model in which the spacecraft is ...

    **ng-Shan Cai, Yang Chen, Jun-Feng Li in Acta Mechanica Sinica (2014)

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    Non-intrusive hybrid interval method for uncertain nonlinear systems using derivative information

    This paper proposes a new non-intrusive hybrid interval method using derivative information for the dynamic response analysis of nonlinear systems with uncertain-but-bounded parameters and/or initial condition...

    Zhuang-Zhuang Liu, Tian-Shu Wang, Jun-Feng Li in Acta Mechanica Sinica (2016)