Add to ORKGMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICROFICHE COPY ALSO AVAILABLE IN AERO LIBRARY.Ten blank pages included in paging.Bibliography: p. 289.by Louis Anthony D'Amario [and] Stephen Patrick Synnott.M.S
A the core of any autonomous rendezvous guidance system must be two algorithms for solving Lambert's...
A new approach for solving Kepler equation for elliptical orbits is developed in this paper. This ne...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Universal solution of Lambert problem for elliptic, parbolic, and hyperbolic motio
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time. ...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Quadratic Newton-Raphson iteration techniques for numerical solutions of Keplers universal transcend...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Kepler's Equation is solved over the entire range of elliptic motion by a fifth-order refinement of ...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. M.S.Micr...
Study compares the use of five different methods for the computer solution of the restricted three-b...
Numerical methods are usually constructed for solving mathematical problems such as differential equ...
A the core of any autonomous rendezvous guidance system must be two algorithms for solving Lambert's...
A new approach for solving Kepler equation for elliptical orbits is developed in this paper. This ne...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Universal solution of Lambert problem for elliptic, parbolic, and hyperbolic motio
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time. ...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Quadratic Newton-Raphson iteration techniques for numerical solutions of Keplers universal transcend...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Kepler's Equation is solved over the entire range of elliptic motion by a fifth-order refinement of ...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. M.S.Micr...
Study compares the use of five different methods for the computer solution of the restricted three-b...
Numerical methods are usually constructed for solving mathematical problems such as differential equ...
A the core of any autonomous rendezvous guidance system must be two algorithms for solving Lambert's...
A new approach for solving Kepler equation for elliptical orbits is developed in this paper. This ne...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...