Download or read book Optimal Transfers Between Close Elliptical Orbits written by Jean Pierre Marec and published by . This book was released on 1969 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA TT F 554 written by J.P. Marec and published by . This book was released on 1969 with total page 265 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Optimal Transfers Between Close Elliptical Orbits with List of References written by and published by . This book was released on 1969 with total page 265 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Minimum impulse Time free Transfer Between Elliptic Orbits written by Frank W. Gobetz and published by . This book was released on 1966 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book OPTIMAL AEROASSISTED ORBITAL TRANSFER INVOLVING ELLIPTICAL ORBITS BALLISTIC FLIGHT PLANE CHANGE DRAG MODULATION COPLANAR DEORBIT written by JENNIE RAE FREELAND JOHANNESEN and published by . This book was released on 1985 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: Minimum-fuel orbital transfer between elliptical orbits is studied by first analyzing separately the three phases of aeroassisted orbital transfer (deorbit, atmospheric fly-through and post atmospheric maneuvers).

Download or read book Survey of Characteristic Velocity Requirements for Two impulse Transfers Between Circular and Coplanar Exterior Elliptical Orbit with Exposition of Local and Overall Optimum Solutions written by Robert Silber and published by . This book was released on 1961 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Optimal Low thrust Limited Power Transfers Between Any Elliptical Orbits written by Jean-Pierre Marec and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Optimal Low thrust Limited Power Transfers Between Arbitrary Elliptical Orbits written by Jean-Pierre Marec and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Optimal Space Trajectories written by Jean-Pierre Marec and published by Elsevier. This book was released on 2012-12-02 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt: Studies in Astronautics, Volume 1: Optimal Space Trajectories focuses on the concept of optimal transfer and the problem of optimal space trajectories. It examines the relative performances of the various propulsion systems (classical and electrical propulsions) and their optimization (optimal mass breakdown), along with parametric and functional optimizations and optimal transfers in an arbitrary, uniform, and central gravitational field. Organized into 13 chapters, this volume begins with an overview of optimal transfer and the modeling of propulsion systems. It then discusses the Hohmann transfer, the Hoelker and Silber bi-elliptical transfer, and the deficiencies of parametric optimization. The book explains the canonical transformation, optimization of the thrust law using the Maximum Principle, and optimal orbit corrections. The time-free orbital transfers and time-fixed orbital transfers and rendezvous are also discussed. Moreover, this volume explains the classical high-thrust and electric low-thrust propulsion systems and rendezvous between two planets. This book is written primarily for engineers who specialize in aerospace mechanics and want to pursue a career in the space industry or space research. It also introduces students to the different aspects of the problem of optimal space trajectories.

Download or read book NASA Technical Translation written by and published by . This book was released on 1969 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1993 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Introduction to the Mathematics and Methods of Astrodynamics written by Richard H. Battin and published by AIAA. This book was released on 1999 with total page 840 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1979 with total page 1504 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Scientific and Technical Reports and Publications for 1969 A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Optimal Plotting of an Elliptical Transfer Orbit Employing Complete Revolutions in the Equatorial Plane of an Axisymmetric Planet written by V. S. Novoselov and published by . This book was released on 1972 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of construction of an elliptical orbit of transition between two orbits with small eccentricities with random and given phases of identical direction motions in the equatorial plane of an axisymmetrical planet is solved. The transition may contain some number of free orbits around the planet and is realized by means of changes of velocity on the initial and final orbits. The problem is solved by the method of approximate solution of variational problems. With accuracy to a small parameter, the transition osculatory ellipse is selected, which minimizes the consumption of fuel for maneuvering. It is assumed that maneuvering is restricted. Equations are derived which allow to determine the optimal orbit of transition. (Author).