Add to ORKGLambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time. ...
Unified form of Lambert theorem for elliptic, hyperbolic, and parabolic orbits based on selecting in...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...
A new universal variable is introduced to improve solution performance for the multiple rev-olution ...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
In this paper, an efficient and simple algorithm is developed for the solution of universal Lambert’...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time. ...
Unified form of Lambert theorem for elliptic, hyperbolic, and parabolic orbits based on selecting in...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...
A new universal variable is introduced to improve solution performance for the multiple rev-olution ...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
In this paper, an efficient and simple algorithm is developed for the solution of universal Lambert’...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
The author has developed a suite of algorithms for solving the perturbed Lambert's problem in celest...
The code solves the single- and multiple-revolution Lambert's Problem (boundary value problem for mo...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Lambert's problem is the two-point boundary-value problem resulting from a two-body orbital transfer...
Classical Lambert's problem is an astrodynamical problem implemented in industrial and scientific so...
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time. ...