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Showing 1 to 7 of 7 for “"Higher Fidelity Model"”.

  1. Coupled Dynamics in the Cislunar Region and Spacecraft Attitude Prediction in a Higher-Fidelity Model​

    … multi-body dynamical environment that cannot be modeled trivially. Traditional point-mass assumptions made to simplify the mission design process may be insufficient for accurately predicting spacecraft motion in environments where orbit-attitude coupling is non-negligible. One of the most famous …

    embry-riddle Repository record for Coupled Dynamics in the Cislunar Region and Spacecraft Attitude Prediction in a Higher-Fidelity Model​ (opens in a new tab)

  2. Study of optical propulsion concepts and techniques for small-satellites

    … thrust generation. This project developed a higher-fidelity model of a recently envisioned small spacecraft propulsion system for precision pointing and proximity control. Plasmonic force propulsion harnesses solar light focused onto plasmon reactive sub-wavelength nanostructures to generate …

    must-thes Repository record for Study of optical propulsion concepts and techniques for small-satellites (opens in a new tab)

  3. A Solution to the Circular Restricted N Body Problem in Planetary Systems

    … on planetary systems, satellite dynamics can be modeled in a fashion similar to the Circular Restricted Three Body Problem (CR3BP) with the Circular Restricted N Body Problem (CRNBP). It was found that this new formulation of the dynamics can then utilize the tools created from all the research …

    calpoly Repository record for A Solution to the Circular Restricted N Body Problem in Planetary Systems (opens in a new tab)

  4. Online Estimation of Unknown Parameters for Flexible Spacecraft

    … of small satellites. However, a high-fidelity model of the flexible mode dynamics is hard to obtain in on-ground testing because not all modes of frequencies can be observed, complicating the controller design. Furthermore, plastic deformations due to long periods of storage of stowed …

    embry-riddle Repository record for Online Estimation of Unknown Parameters for Flexible Spacecraft (opens in a new tab)

  5. Autonomous optimal trajectory design employing convex optimization for powered descent on an asteroid

    … cannot be represented by a constant gravity model nor a Newtonian model. The trajectory design algorithm needs to be robust and efficient to guarantee a designed trajectory and complete the calculations in a reasonable time frame.</p> <p>This research investigates the following questions: Can …

    iastate Repository record for Autonomous optimal trajectory design employing convex optimization for powered descent on an asteroid (opens in a new tab)

  6. Uncertainty-Integrated Surrogate Modeling for Complex System Optimization

    <p>Approximation models such as surrogate models provide a tractable substitute to expensive physical simulations and an effective solution to the potential lack of quantitative models of system behavior. These capabilities not only enable the efficient design of complex systems, but is also …

    syracuse-diss Repository record for Uncertainty-Integrated Surrogate Modeling for Complex System Optimization (opens in a new tab)