Synonyme wurden verwendet für: dynamics
Suche ohne Synonyme: keywords:(dynamics of spacecraft ‐ and Newtonian dynamics)

1–19 von 19 Ergebnissen
|

    Dynamics of Spacecraft

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

    Cylindrical orthogonal norm-based stochastic collision risk measures in spacecraft formation flying

    Núñez Garzón, Ulises E. / Lightsey, E. Glenn | Elsevier | 2023
    Schlagwörter: Spacecraft formation flying , Spacecraft stochastic collision risk , Spacecraft collision avoidance , Spacecraft collision risk assessment , Spacecraft collision risk management , Spacecraft collision risk interpretation and decision-making , Probability of collision , Relative orbital dynamics

    A Spaceborne Design and Airborne Demonstration of Digitally-Beamformed Antennas for SweepSAR Imaging

    Sadowy, Gregory / Chamberlain, Neil / Hensley, Scott et al. | NTRS | 2011
    Schlagwörter: Deformation Ecosystem??Structure Dynamics of Ice (DESDynl) , Spacecraft Design, Testing And Performance , Communications And Radar

    Optimal Spacecraft Attitude Control

    Tewari, Ashish | Wiley | 2011
    Schlagwörter: spacecraft control torques ‐ applied to spacecrafts , optimal spacecraft attitude control , rocket thrusters, and spacecraft ‐ reaction control system (RCS), and attitude thrusters , spacecraft, desired orientation ‐ attitude stability, and spacecraft control , extremal angular velocity ‐ for multi‐axis spin maneuver of spacecraft , tracking control of satellite attitude dynamics , spacecraft, environmental disturbances ‐ and control torques , satellite dynamics plant for tracking control ‐ and nadir pointing, attitude control system , multi‐axis rotational maneuvers of spacecraft ‐ optimal control, end‐point constraints

    Spacecraft Dynamics Employing a General Multi-tank and Multi-thruster Mass Depletion Formulation

    Panicucci, Paolo / Allard, Cody / Schaub, Hanspeter | Springer Verlag | 2018
    Schlagwörter: Equations of motion , Spacecraft dynamics , Aerospace Technology and Astronautics , Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics)

    Target-Based Guidance Method for Trajectories with Multiple Flybys

    Giordano, Carmine / Varga, Gabor / Mackenzie, Ruaraidh et al. | AIAA | 2023
    Schlagwörter: Moons of Jupiter , Spacecraft Trajectories , Flight Dynamics , Guidance and Navigational Algorithms , Guidance, Navigation, and Control Systems

    Passivity-Based Adaptive Finite-Time Trajectory Tracking Control for Spacecraft Proximity Operations

    Sun, Liang | AIAA | 2015
    Schlagwörter: Autonomous Rendezvous and Docking , Target Spacecraft , Six Degree of Freedom , Attitude Dynamics

    Kestrel Results at Liftoff Conditions for a Space Launch System Configuration in Proximity to the Launch Tower

    Steven E Krist / Nalin A Ratnayake / Farhad Ghaffari et al. | NTRS | 2019
    Schlagwörter: Computational fluid dynamics , Spacecraft Design, Testing And Performance , Angle of attack

    Ground Segment

    Chatel, Franck | Wiley | 2011
    Schlagwörter: flight dynamics, experts ‐ in close liaison with satellite manufacturer , antennas, communication interface ‐ with spacecraft , communication links, ground stations and control centre ‐ ‘glue’ of mission , spacecraft operations ‐ operations engineers’ tasks in preparatory phase , flight operations system ‐ in charge of conducting operations , In‐Orbit Tests (IOT) and telecommunication missions , data processing, chain of ground station ‐ compatibility with spacecraft , ground segment, and European Cooperation for Space Standardization (ECSS) institution

    Mission Analysis

    Stark, John P. W. / Swinerd, Graham G. | Wiley | 2011
    Schlagwörter: mission analysis ‐ celestial mechanics and spacecraft's dynamics , spacecraft launch time , mission analysis, ‘front‐end’ systems level activity ‐ and celestial mechanics , two principal constraints ‐ design of aeromanoeuvring vehicle , interplanetary missions for interplanetary spacecraft , missions, categories ‐ Low Earth Orbit (LEO), MEO, GEO, HEO and non‐geocentric orbits

    Celestial Mechanics

    Stark, John P. W. / Swinerd, Graham G. / Fortescue, Peter W. | Wiley | 2011
    Schlagwörter: atmospheric drag ‐ for low Earth‐orbiting spacecraft , 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 , Kepler's equation, simple relationship ‐ time and position , theory of celestial mechanics ‐ motion of a spacecraft prediction

    Attitude Control of Rockets

    Tewari, Ashish | Wiley | 2011
    Schlagwörter: guidance and control system ‐ for a rocket , attitude control of rockets ‐ for launch vehicle, aerodynamic load consideration , roll control system of launch vehicle ‐ reaction jet controlled, single‐axis spacecraft , pitch control of rockets ‐ pitch and yaw control of launch vehicle, and zero angle of attack , launch vehicle, operation ‐ speeds and altitudes , attitude control plant, of a rocket ‐ and zero angle of attack and sideslip , aerodynamic parameters ‐ for gravity‐turn rocket's pitch dynamics plant , pitch‐yaw aerodynamic symmetry ‐ by launch vehicles, and ballistic missiles , yaw control of rockets ‐ a feedforward path, not required in yaw control

    Suboptimal LQR-based spacecraft full motion control: Theory and experimentation

    Guarnaccia, Leone / Bevilacqua, Riccardo / Pastorelli, Stefano P. | Elsevier | 2016
    Schlagwörter: Advanced Autonomous Multiple Spacecraft , guidance dynamics corporation , intelligent battery and power system , Office of Naval Research , spacecraft , Spacecraft , Six-degree-of-freedom

    Feasibility of Determining Aerodynamic Coefficients for a NASA Apollo Body With the Use of Telemetry Data From Free Flight Range Testing

    B. Topper / T. G. Brown / E. Bukowski et al. | NTIS | 2007
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Test and evaluation , Center of gravity , Dynamics , Manned spacecraft

    Optimal Re-Entry Trajectory Terminal State Due to Variations in Waypoint Locations

    W. J. Karasz | NTIS | 2008
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Spacecraft Trajectories & Flight Mechanics , Numerical methods and procedures , Calculus of variations

    Carina Aerothermal Test at Mach 8

    M. G. Hammond | NTIS | 1991
    Schlagwörter: Missile Trajectories & Reentry Dynamics , Angle of attack , Spacecraft , Test and evaluation

    Analysis of NASA's Post-Challenger Response and Relationship to the Columbia Accident and Investigation

    R. G. Gregory / S. J. Marcellino / S. A. Moyer | NTIS | 2006
    Schlagwörter: Manned Spacecraft , Group dynamics , Nasa(National aeronautics and space administration) , Normalization of deviance , Assumption of risk

    An attitude model for the spacecraft of the ESA mission Gaia

    Keil, R. / Risquez, D. / van Leeuwen, F. et al. | Elsevier | 2011
    Schlagwörter: centre of mass , data processing and analysis consortium , end of life , field(s) of view , line(s) of sight , multiple-input and multiple-output , Runge–Kutta integrator algorithm of 4th order , (mechanical) spacecraft reference system , single-input and single-output , Spacecraft , Dynamics

    Significance of 3U CubeSat OrigamiSat-1 for space demonstration of multifunctional deployable membrane

    Ikeya, Kosuke / Sakamoto, Hiraku / Nakanishi, Hiroki et al. | Elsevier | 2020
    Schlagwörter: Gossamer spacecraft , Deployment dynamics , communication and inhibit control board , Tokyo Institute of Technology