OPTIMUM SATELLITE LAUNCHER TRAJECTORY GUIDED WITH PROPORTIONAL NAVIGATION PLUS GRAVITY COMPENSATION GUIDANCE

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Published: 2006-12-01
DOI: https://doi.org/10.31026/j.eng.2006.04.04

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Waleed Kh. Al-Ashtari

Abstract

The optimum trajectory of a single or multi-stage satellite launcher guided with proportional
navigation guidance (PNG) is addressed. The PNG is extended to compensate for the gravity effect.
For the trajectory optimization problem, the launcher is modeled as a mass point flying around the
center of the Earth. To provide a completely valid analysis, all known influences on the launcher
trajectory have been considered; Empirical equations have been used in order to model the Earth
standard atmosphere in SI units. A computer program had been constructed in order to simulate the
trajectory of such launcher from the available initial conditions. Pegasus launcher is used as a
hypothetical example. The simulator results show that the proportional navigation plus gravity
compensation guidance gives fairly accurate results.

Article Details

Issue

Vol. 12 No. 04 (2006): Journal of Engineering

Section

Articles
Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

 
 

How to Cite

“OPTIMUM SATELLITE LAUNCHER TRAJECTORY GUIDED WITH PROPORTIONAL NAVIGATION PLUS GRAVITY COMPENSATION GUIDANCE” (2006) Journal of Engineering, 12(04), pp. 916–928. doi:10.31026/j.eng.2006.04.04.

References

Bong Wie “Space Vehicle Dynamics and Control”, AIAA, Inc., 1998.

Encyclopedia Britannica, 2002.

Joseph Asher, and Isaac Yaesh, “Advance in Missile Guidance Theory”, Vol.180; 1998.

Katsuhiko Ogata, “Modern Control Engineering”, 4th Edition, 2002.

Mayrhofer M, and. Sachs G, “Orbital Stage Abort Trajectories after Separation from Carrier”, Proc-12 th, International Symposium on Space Flight Dynamics, ESOC, Darmstadt, Germany, pp. 463- 469, June 1997.

Meriam J.L., and Kraige L.G., “Dynamics”; Vol.2, 4th Edition, 1998.

Paul Zarchan ,“Tactical and Strategic Missile Guidance”, Vol.124; 1990.

Steven J. Isakowitz, Joseph P. Hopkins Jr., and Joshua B. Hopkins: “Pegasus”; Space Launch System, International Reference Guide to Space Launch, AIAA, pp. 267-279; 1999.