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    An application of the mechanical rotation scheme to an analysis of the motion of flying objects

    Grevtsov, N / Melts, I / Sazonov, D et al. | SAGE Publications | 2005
    Keywords: equations of motion of rigid bodies , trajectory

    Trajectory optimization of hypersonic vehicle considering the quasi-static assumption of pitch motion

    Ma, Shoudong / Yang, Yuxin / Yang, Hua et al. | Elsevier | 2024
    Keywords: Quasi-static assumption of pitch motion , Trajectory optimization

    Trajectory Planning for CubeSat Short-Time-Scale Proximity Operations

    Kobilarov, Marin / Pellegrino, Sergio | AIAA | 2014
    Keywords: Motion Planning , Four Degree of Freedom , Trajectory Optimization

    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

    Stable Nonlinear Feedback Control Using Quaternionic Orbital Elements

    Kelly, Patrick / Majji, Manoranjan / Junkins, John L. | AIAA | 2023
    Keywords: Trajectory Optimization , Argument of Latitude , Kepler's Laws of Planetary 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

    Generalized Shape Expansion-Based Motion Planning in Three-Dimensional Obstacle-Cluttered Environment

    Zinage, Vrushabh Vijaykumar / Ghosh, Satadal | AIAA | 2020
    Keywords: Motion Planning , Six Degree of Freedom , Trajectory Optimization

    Information-Based Guidance and Control Architecture for Multi-Spacecraft On-Orbit Inspection

    Nakka, Yashwanth Kumar / Hönig, Wolfgang / Choi, Changrak et al. | AIAA | 2022
    Keywords: Motion Planning , Three Degrees of Freedom , Trajectory Optimization

    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

    Transfers Between Moons with Escape and Capture Patterns via Lyapunov Exponent Maps

    Canales, David / Howell, Kathleen C. / Fantino, Elena et al. | AIAA | 2023
    Keywords: Moons of Jupiter , Low Energy Trajectory , Kepler's Laws of Planetary Motion

    D Matrix for Keplerian State Error Propagation

    Bombardelli, Claudio / Hernando-Ayuso, Javier / Armellin, Roberto | AIAA | 2024
    Keywords: Trajectory Optimization , Kepler's Laws of Planetary Motion

    Investigation of Stable Regions of Spacecraft Motion in Binary Asteroid Systems by Terminal Condition Maps

    Li, Xiangyu / Qiao, Dong / Jia, Feida | Springer Verlag | 2021
    Keywords: Stability of motion , Trajectory design

    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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