초록 ▼

A system and method for orbital planning allows iterative calculations of orbital parameters to be accomplished in an automated way with one parameter solution serving as input to the next parameter's calculation. A software program employs a graphical user interface (GUI) to allow a space mission a

A system and method for orbital planning allows iterative calculations of orbital parameters to be accomplished in an automated way with one parameter solution serving as input to the next parameter's calculation. A software program employs a graphical user interface (GUI) to allow a space mission analyst to set up a series of sub-problems of any desired level of complexity. The program then implements the series automatically and sequentially, incorporating the solution to one sub-problem into the input to the next.

대표청구항 ▼

1. A method for profiling and solving space mission problems, the method comprising:creating a space mission analysis scenario;setting up a control sequence that simulates a problem to be solved in the space mission;selecting control variables to be checked in solving the problem;identifying paramet

1. A method for profiling and solving space mission problems, the method comprising:creating a space mission analysis scenario;setting up a control sequence that simulates a problem to be solved in the space mission;selecting control variables to be checked in solving the problem;identifying parameters to be used in defining desired results that represent an adequate solution to the problem;establishing profiles for each particular sub-problem of the problem to be solved by:specifying which of the previously selected control variables should be varied for each particular sub-problem, andspecifying what results should be achieved for each particular sub-problem; andrunning simulations for each of the established profiles to provide a result representing a solution to the problem to be solved.2. The method of claim 1, wherein the step of running simulations for each of the established profiles comprises:after each profile is run, collecting the solution to that profile, and, in the event that there is a subsequent profile to be run, applying it as the initial starting point for a subsequent profile; andcollecting the solution to the last profile and providing it as the result representing a solution to the problem to be solved.3. A computer system adapted to perform profiling and solving space mission problems for which a space mission analysis scenario has been created, the system comprising:a processor;a memory, addressable by the processor, including software instructions adapted to enable the computer system to perform the steps of:setting up a control sequence that simulates a problem to be solved in the space mission;selecting control variables to be checked in solving the problem;identifying parameters to be used in defining desired results that represents an adequate solution to the problem;establishing profiles for each particular sub-problem of the problem to be solvedspecifying which of the previously selected control variables should be varied for each particular sub-problem, andspecifying what results should be achieved for each particular sub-problem; andrunning simulations for each of the established profiles to provide a result representing a solution to the problem to be solved.4. The computer system of claim 3, wherein the step of running simulations for each of the established profiles comprises:after each profile is run, collecting the solution to that profile, and, in the event that there is a subsequent profile to be run, applying it as the initial starting point for a subsequent profile; andcollecting the solution to the last profile and providing it as the result representing a solution to the problem to be solved.5. A computer program product for enabling a computer to perform profiling and solving space mission problems for which a space mission analysis scenario has been created, the computer program product comprising:software instructions for enabling the computer to perform predetermined operations, anda computer readable medium embodying the software instructions;the predetermined operations including the steps of:setting up a control sequence that simulates a problem to be solved in the space mission;selecting control variables to be checked in solving the problem;identifying parameters to be used in defining desired results that represents an adequate solution to the problem;establishing profiles for each particular sub-problem of the problem to be solved by:specifying which of the previously selected control variables should be varied for each particular sub-problem; andspecifying what results should be achieved for each particular sub-problem; andrunning simulations for each of the established profiles to provide a result representing a solution to the problem to be solved.6. The computer program product of claim 5, wherein the step of running simulations for each of the established profiles comprises:after each profile is run, collecting the solution to that profile, and, in the event that there is a subsequent profile to be run, applying it as the initial starting point for a subsequent profile; andcollecting the solution to the last profile and providing it as the result representing a solution to the problem to be solved.