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Showing 1 to 20 of 129 for “"Rendezvous"”.

  1. Rendezvous: Stories and a Novella

    <p>People are often a product of their environment, and each of the characters in this collection is an example of that shaping effect. These stories take you to the southern plains–land of red dirt, Bluestem, and prairie wind. Themes like hope, loss, and the exploration of frontier appear …

    uno Repository record for Rendezvous: Stories and a Novella (opens in a new tab)

  2. Optimal cooperative power-limited rendezvous

    Minimum-fuel rendezvous of two power-limited low-thrust spacecraft is investigated. Both vehicles are active and provide thrust to complete the rendezvous. Total propellant consumption is minimized. Two gravitational field models are investigated: the Clohessy-Wiltshire linearized field and the …

    uiuc Repository record for Optimal cooperative power-limited rendezvous (opens in a new tab)

  3. Symmetric rendezvous problem with overlooking

    cambridge

  4. Optimal multiple-impulse orbital rendezvous.

    Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.

    mit Repository record for Optimal multiple-impulse orbital rendezvous. (opens in a new tab)

  5. Robust rendezvous maneuver point conditions

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.

    mit Repository record for Robust rendezvous maneuver point conditions (opens in a new tab)

  6. Optimal cooperative time-fixed impulsive rendezvous

    … trajectories for the fixed-time cooperative rendezvous of two spacecraft. The method assumes that the vehicles perform a minimum of three impulsive maneuvers with each vehicle being active, that is, making at least one maneuver. The cost of a reference rendezvous solution is improved by an …

    uiuc Repository record for Optimal cooperative time-fixed impulsive rendezvous (opens in a new tab)

  7. Rendezvous approach guidance for uncooperative tumbling satellites

    The development of a Rendezvous and Proximity Operations (RPO) guidance algorithm for approaching uncooperative tumbling satellites has multiple purposes including on-orbit satellite servicing, space debris removal, asteroid mining, and on-orbit assembly. This thesis develops a guidance algorithm …

    mit Repository record for Rendezvous approach guidance for uncooperative tumbling satellites (opens in a new tab)

  8. Autonomous orbital rendezvous using angles-only navigation

    This study assesses navigation performance for rendezvous and close approach applications where on-board navigation must be accomplished through the use of angles-only measurements by developing various relative motion orbital trajectories. Chaser vehicle maneuvers designed to enhance the …

    mit Repository record for Autonomous orbital rendezvous using angles-only navigation (opens in a new tab)

  9. Fuel optimal rendezvous including a radial constraint

    Fuel-optimal rendezvous in orbit is examined using thrust-impulses and coasting arcs. Necessary conditions for the optimality of fuel-optimal rendezvous with and without radial constraints are derived. These conditions are then used to verify the optimality of trajectories obtained from a …

    vt Repository record for Fuel optimal rendezvous including a radial constraint (opens in a new tab)

  10. Optimization of Active Rendezvous Trajectories by Genetic Algorithms

    … UnderWater Vehicles (UWV) trajectories and rendezvous trajectories of continuous low-thrust spacecraft are examined. One of the methods to solve such problems is the Genetic Algorithm (GA) method. In this work, a GA has been developed using Matlab®. It treats possible solutions to the …

    embry-riddle Repository record for Optimization of Active Rendezvous Trajectories by Genetic Algorithms (opens in a new tab)

  11. Cooperative Power-Limited Optimal Rendezvous Between Many Spacecraft

    <p>The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring either a circular or an elliptic orbit is investigated. Both cooperative and non cooperative maneuvers are studied. The maximum principle of Pontryagin is applied to the optimal control rendezvous

    embry-riddle Repository record for Cooperative Power-Limited Optimal Rendezvous Between Many Spacecraft (opens in a new tab)

  12. Orbital rendezvous using an Augmented Lambert Guidance scheme

    The development of an Augmented Lambert Guidance Algorithm that matches the position and velocity of an orbiting target spacecraft is presented in this thesis. The Augmented Lambert Guidance Algorithm manipulates the inputs given to a preexisting Lambert guidance algorithm to control the boost of a …

    mit Repository record for Orbital rendezvous using an Augmented Lambert Guidance scheme (opens in a new tab)

  13. Optimal Control of Co-Operative Systems--the Rendezvous Problem

    Made available in DSpace on 2014-12-08T22:23:40Z (GMT). No. of bitstreams: 1 6503587.pdf: 1280423 bytes, checksum: c7275e1f249c4f3e89a8f00ec46293f0 (MD5) Previous issue date: 1964

    uiuc Repository record for Optimal Control of Co-Operative Systems--the Rendezvous Problem (opens in a new tab)

  14. Efficient algorithms for risk-averse air-ground rendezvous missions

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2022-04-06 without embargo terms

    uiuc Repository record for Efficient algorithms for risk-averse air-ground rendezvous missions (opens in a new tab)

  15. Near Earth orbit determination and rendezvous navigation using GPS

    Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1986

    mit Repository record for Near Earth orbit determination and rendezvous navigation using GPS (opens in a new tab)

  16. Line-of-sight guidance techniques for manned orbital rendezvous

    Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1963.

    mit Repository record for Line-of-sight guidance techniques for manned orbital rendezvous (opens in a new tab)

  17. Planning and scheduling proximity operations for autonomous orbital rendezvous

    … scheduling problem for autonomous orbital rendezvous. The algorithm of this thesis allows the operator to specify planned modes, which encode the chase satellite's operations. The scheduler optimally places these modes in the midst of the environmental conditions that fall out of the chase …

    mit Repository record for Planning and scheduling proximity operations for autonomous orbital rendezvous (opens in a new tab)

  18. Six degree of freedom optimal trajectories for satellite rendezvous

    … with no imposed constraint on the time of the rendezvous. Further solutions are then found by varying the vehicle center of gravity location along one axis, thereby coupling the rotational motions into two axes of translation thrusters, and by imposing time limits on the rendezvous. A …

    vt Repository record for Six degree of freedom optimal trajectories for satellite rendezvous (opens in a new tab)

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