Add to ORKGComputer program for transfer orbit trajectory optimization based on Lagrange multipliers, Newton-Raphson method, and power serie
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Presented to the 11th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at ...
Equations of motion for two dimensional digital computer program for calculation of optimum trajecto...
"A computer program has been designed which determines the minimum-burn-time, thrusting, transfer tr...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
This report describes the current state of development of methods for calculating optimal orbital tr...
AbstractThis article presents a systematic direct approach to carry out effective optimization of a ...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
This paper proposes a systematic direct approach to carry out effective multi-objective optimization...
The problem of many revolution low-thrust Earth-orbit trajectory optimization is considered. The obj...
Computer program using numerical methods that calculates minimum time for space vehicle to meet its ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
AbstractLow-thrust Earth-orbit transfers with 10−5-order thrust-to-weight ratios involve a large num...
Trajectory optimization and linearized pitch computer program for Scout launch vehicl
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Presented to the 11th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at ...
Equations of motion for two dimensional digital computer program for calculation of optimum trajecto...
"A computer program has been designed which determines the minimum-burn-time, thrusting, transfer tr...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
This report describes the current state of development of methods for calculating optimal orbital tr...
AbstractThis article presents a systematic direct approach to carry out effective optimization of a ...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
This paper proposes a systematic direct approach to carry out effective multi-objective optimization...
The problem of many revolution low-thrust Earth-orbit trajectory optimization is considered. The obj...
Computer program using numerical methods that calculates minimum time for space vehicle to meet its ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
AbstractLow-thrust Earth-orbit transfers with 10−5-order thrust-to-weight ratios involve a large num...
Trajectory optimization and linearized pitch computer program for Scout launch vehicl
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Presented to the 11th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at ...
Equations of motion for two dimensional digital computer program for calculation of optimum trajecto...