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    Optimization of Whole-Body Motion for Humanoid Robot Walking Down Stairs with Small Joint Range of Motion

    Meng, Xiang / Huang, Zelin / Liang, Qian et al. | Springer Verlag | 2023
    Keywords: Motion generation , Trajectory optimization , Limited joint range of motion

    Dynamics of Spacecraft

    Fortescue, Peter W. / Swinerd, Graham G. | Wiley | 2011
    Keywords: moment‐of‐momentum , general attitude dynamics ‐ mathematically identical to trajectory dynamics , attitude motion of specific types of spacecraft ‐ and bias , trajectory dynamics , dynamics of translation and rotation ‐ interpreting momenta , dynamics of spacecraft ‐ and Newtonian dynamics

    Optimal Trajectory Control of Morphing Aircraft in Perching Maneuvers

    Wickenheiser, Adam M. / Garcia, Ephrahim | Wiley | 2012
    Keywords: concept of perching, in ISR missions , optimal trajectory, perching maneuvers , vehicle, equations of motion , trajectory optimization, in perching

    Parametric Studies of an Un-Guided Rocket Using Simple Point-Mass Trajectory Simulation Model

    Panwar, Mardav / Gorrepati, Srinivasa Rao / Chauhan, Manish Kumar | Springer Verlag | 2024
    Keywords: Point mass—trajectory simulation model (PM-TSM) , Equations of motion for point mass model

    Celestial Mechanics

    Stark, John P. W. / Swinerd, Graham G. / Fortescue, Peter W. | Wiley | 2011
    Keywords: hyperbolic trajectory , two‐body problem—particle dynamics ‐ motion of two co‐rotating point masses , celestial mechanics ‐ and theory, spacecraft's orbital motion , mutual gravitational force of attraction ‐ between any two bodies , theory of celestial mechanics ‐ motion of a spacecraft prediction

    Optimal Guidance of Rockets

    Tewari, Ashish | Wiley | 2011
    Keywords: optimal guidance of rockets ‐ time‐varying parameters, of equations of motion , fast response times ‐ in translation and rotation of rockets , translational motion of center of mass ‐ of flight vehicle, in vertical plane , vertical launch of a rocket (Goddard's Problem) ‐ rocket flight for a vertical launch , robust and adaptive guidance ‐ changing trajectory of a rocket, precluding real‐time computation by linear time‐invariant (LTI) approximation

    Spacecraft Guidance Systems

    Tewari, Ashish | Wiley | 2011
    Keywords: small magnitude of perturbations ‐ atmospheric drag, modifying trajectory , two spherical body, relative motion ‐ mutual gravitational attraction, orbital mechanics , Hyperbolic Orbit, equivalent form of Kepler's equation ‐ hyperbolic anomaly, H

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