Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem

Details Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem

Jan 2011

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2011aas...21725415n&link_type=abstract

American Astronomical Society, AAS Meeting #217, #254.15; Bulletin of the American Astronomical Society, Vol. 43, 2011

Other

Scientific paper

In this study, the main discussion emphasizes on the spacecraft operation with a concentration on stationary points in space. To achieve these objectives, the circular restricted problem was solved for selected approaches. The equations of motion of three body restricted problem was demonstrated to apply in cases other than Lagrange's (1736-1813 A.D.) achievements, by means of the purposed CN (Cyrus Nejat) theorem along with appropriate comments. In addition to five Lagrange, two other points, CN1 and CN2 were found to be in unstable equilibrium points in a very large distance respect to Lagrange points, but stable at infinity. A very interesting simulation of Milky Way Galaxy and Andromeda Galaxy were created to find the Lagrange points, CN points (Cyrus Nejat Points), and CN lines (Cyrus Nejat Lines). The equations of motion were rearranged such a way that the transfer trajectory would be conical, by means of decoupling concept. The main objective was to make a halo orbit transfer about CN lines. The author purposes therefore that all of the corresponding sizing design that they must be developed by optimization techniques would be considered in future approaches. The optimization techniques are sufficient procedures to search for the most ideal response of a system.

Affiliated with

Also associated with

No associations

Rating

Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Space Instrument Optimization by Implementing of Generic Three Bodies Circular Restricted Problem will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1399677