Dilmurat Azimov
azimov [ at ] mail.utexas.edu

Publications, 1988 -

D.M. Azimov. On the question of optimality of the intermediate thrust arcs./ Algorithms and numerical methods of solutions of problems of the computational and applied mathematics. / Tashkent State University. Tashkent. 1988. pp.6-9.

D.M. Azimov. On the definition of the optimal trajectories in a linear central field. / UzNIINTI. N.887-Uz.88. Tashkent. 1988. 22 p.

D.M. Azimov. On the question of structure of the optimal trajectories in a linear central field. / UzNIINTI. N.1160-Uz.89. Tashkent. 1989. 23 p.

D.M. Azimov. A study of the optimal trajectories in the central Newtonian field. / Autoreferat of Candidate Dissertation. Moscow. University of People Friendship. 1991. 14 p.

D.M. Azimov. On the question of definition of points of switching over on the optimal trajectories. / Controllable Systems. Tashkent State University. 1992. pp.18-20.

D.M. Azimov. Some analytical solutions for rocket motion with intermediate thrust force in a Newtonian field. / International Scientific and Practical Conference "The Problems of Mechanics and Machinery". Tashkent. May 25-27, 1993. pp.88.

D.M. Azimov. On the problem of optimal transfer between elliptical orbits. / Proceedings of the Scientific Conference "Mechanics and its applications". Tashkent. November 9-11, 1993. pp. 6.

D.M. Azimov. , N.A. Korshunova. Selected Lectures on Theory of the Stability of Motion. Textbook for undergraduate students of the Mechanical and Mathematical Faculties. Tashkent State University. 1995. 32 p.

D.M. Azimov. Analytical solutions for intermediate thrust arcs of rocket trajectories in a Newtonian field. / Pricladnaja matematica i mehanica. Moscow, Russia. Nauka. 1996. N.63., pp.74-80.

Translation: D.M. Azimov. Analytical solutions for intermediate thrust arcs of rocket trajectories in a Newtonian field. / Journal of Applied Mathematics and Mechanics. Pergamon. USA. Vol.60, No.3, pp.421-427. 1996.

D.M. Azimov. Some results of analysis of the intermediate thrust arcs in Mayer's variational problem. / The first scientific- practical conference "Space research, technology and conversion". Scientific Engineering Complex of SPA "Koinot". Tashkent. April 11-12, 1996, pp.40.

D.M. Azimov, E. Mirmakhmudov. Regarding the analysis of possibilities of changing asteroids' orbits./ Abstracts. International conference "Asteroid Hazard-96". Sankt-Peterburg. Russia. July 14-19. 1996.

D.M. Azimov, B.I. Musabekov. A new analytical solution for maximum thrust arcs and their application to optimal transfer between coplanar orbits. / AIA '96. Proceedings of the Ankara International Aerospace Conference and Symposia, Ankara, Turkey. Sept. 19-21, 1996, pp.193-200.

D.M. Azimov. Some classes of motion trajectory with intermediate thrust arcs in the Newtonian field. / Proceedings of the International Conference on Analytical and Applied Mechanics. Tashkent. Sept. 26-29, 1996, pp.8-10.

D.M. Azimov, E. Mirmakhmudov, T.A. Samusenko. On the program providing for direct and indirect problems of definitions of the orbital elements by observations. / Proceedings of the International Conference on "Problems of Celestial Mechanics". Sankt-Peterburg. Russia. June 3-6, 1997, pp. 31-34.

D.M. Azimov, E. Mirmakhmudov, T.A. Samusenko. Definition of preliminary orbital elements of the small bodies of solar system by Gauss method. / Scientific-Practical Conference "Space Research, Technology and Conversion - II". Scientific Engineering Complex of State Production Association "Koinot". Uzbek State Space Research Agency "Uzbekkosmos". Tashkent. April 16-17, 1997, pp.46-48.

D.M. Azimov. On One Class of Optimum Spherical Trajectories in a Newtonian Field / Scientific - Practical Conference "Space Research, Technology and Conversion - II". Scientific Engineering Complex of SPA "Koinot". Uzbek State Space Research Agency "Uzbekkosmos". Tashkent. April 16-17, 1997, pp.35-37.

D.M. Azimov., O.B. Rakhimov. On the Problem of Maximum Range Trajectories of Air-to-Surface Missile. / Scientific - Practical Conference "Space Research, Technology and Conversion - II". Scientific Engineering Complex of SPA "Koinot". Uzbek State Space Research Agency "Uzbekkosmos ". Tashkent. April 16-17, 1997, pp.74-76.

D.M. Azimov. Some classes of spiral trajectories for motion with intermediate thrust in a Newtonian field. / Proceedings of the International Conference on Applied Mathematics and Mechanics. Samarkand. Uzbekistan. 18-22-November, 1997. pp.92-99.

D.M. Azimov. An integration of Hamilton-Jacoby equation for intermediate thrust arcs by methods of analytical mechanics. / Problems of Mechanics. Academy of Sciences of Uzbekistan. Tashkent. No.1. 1998, pp.3-7.

D.M. Azimov. Optimal analytic classes of trajectories of motion with intermediate thrust arc in Mayer variational problem. / The Program of the Scientific - Practical Conference "Space research, technology and conversion - III". Uzbek State Space Research Agency "Uzbekkosmos". Tashkent. June 3-5, 1998.

D.M. Azimov, E Mirmakhmudov, T.I. Samusenko. Using of DE200/LE200 ephemerides for taking into account perturbations from the Moon and Sun in calculating of satellite's trajectory. / The Program of the Scientific - Practical Conference "Space research, technology and conversion ­ III". Uzbek State Space Research Agency "Uzbekkosmos ". Tashkent. June 3-5, 1998.

D.M. Azimov, E Mirmakhmudov, T.I. Samusenko. Calculation of satellite's trajectory taking into account perturbations from higher order zonal, tesseral and sectorial harmonics. / The Program of the Scientific - Practical Conference "Space research, technology and conversion - III". Uzbek State Space Research Agency "Uzbekkosmos ". Tashkent. June 3-5, 1998.

D.M. Azimov. The intermediate thrust arcs of trajectories of a point with changing mass in a linear central field. / Problems of Mechanics. Academy of Sciences of Uzbekistan. Tashkent. 1998. N.6, pp. 6 -11.

D.M. Azimov. On one class of maximum thrust arcs in Mayer's variational problem. / Problems of Mechanics. Academy of Sciences of Uzbekistan. Tashkent. 1999. N.2, pp. 3-9.

D.M. Azimov. Six classes of trajectories of motion with intermediate thrust arc. Reports of the Academy of Sciences of Uzbekistan. Tashkent. 1999. N.2, pp. 13-16.

Azimov, D. M., New Classes for Intermediate-Thrust Arcs of Flight Trajectories in a Newtonian Field. Journal of Guidance, Control and Dynamics. AIAA. 2000, Vol.23, N.1, pp.142-145.

D.M. Azimov. Uchastki promejutochnoy tyagi v variac'ionnoy zadache Mayera. T.64. Vyp.1, 2000. pp. 92-101. Prikladnaya matematika i mehanika. Nauka. Russia. Translation: Intermediate thrust arcs in Mayer's variational problem. Journal of Applied Mathematics and Mechanics. Pergamon. USA. Vol.64, No.1, pp.87-95. 2002.

Bishop, R.H. and Azimov, D.M., New Analytic Solutions to the Fuel-Optimal Orbital Transfer Problem using Low-Thrust Exhaust Modulated Propulsion. / AAS/AIAA Space Flight Mechanics Meeting. Paper AAS 00-131. 23-26 January, 2000. Clearwater, FL.

Azimov, D.M., and Bishop, R.H. Analytic Solution to the Problem of Turning of an Elliptic Orbital Plane via Spherical Intermediate Thrust Arc. AAS/AIAA Space Flight Mechanics Meeting. Paper AAS 00-208. January 23-26, 2000. Clearwater, Florida.

Azimov, D.M., and Bishop, R.H. Earth-Mars Minimum Fuel Trajectories via Circular and Spiral Low Thrust Arcs. NASA JSC/A&M/UT Meeting. 26 p. Texas A&M University, College Station, Texas. USA. December 1, 2000.

Bishop, R.H. and Azimov, D.M., Analytical Trajectories for Extremal Motion With Low-Thrust Exhaust-Modulated Propulsion. Journal of Spacecraft and Rockets. AIAA. 2001, Vol.38, N.6, pp. 897-903.

Bishop, R.H., Azimov, D.M., W.T. Fowler., VASIMR-Class Analytic Guidance. Preliminary investigations on optimal trajectories. Presentation at NASA JSC/UT Meeting.Advanced Space Propulsion Laboratory., p.17, NASA Lyndon Johnson Space Center. January 18, 2001.

Azimov, D.M., and Bishop, R.H., Extremal Rocket Motion with Maximum Thrust in a Linear Central Field. Journal of Spacecraft and Rockets. AIAA. 2001. Vol. 38, N.5. pp.765-776.

Bishop, R.H., Azimov, D.M., Dawn, T., DeRidder, M., Braden, E., Vadali, S., Aroonwilairut, K., Condon, G., Crain, T. Mars Sample Return: The SEP Earth Return. 43 p. NASA JSC. Houston. USA. July 13, 2001.

Bishop, R.H., Azimov, D.M., Ocampo, C., Condon, G., Crain, T., Dawn, T., Braden., E., Vadali, S., Aroonwilairut, K. Low Thrust Trajectory Work at JSC. Presented to the Mars Program Systems Engineering Team. 48 p. NASA JSC. Houston. USA. December 5, 2001.

Azimov, D.M., and Bishop, R.H., Planetary Capture Using Low-Thrust Propulsion, 16th International Symposium on Space Flight Dynamics. Pasadena, California. USA. December 3-6, 2001. 31 p.

Azimov, D.M., and Bishop, R.H. New Classes of Optimal Space Trajectories. pp.1-10. IAC-02-A.6.01. 53rd Congress of International Astronautical Federation. The World Space Congress 2002. October 10-19, 2002. 10 p.

Azimov, D.M., and Bishop, R.H. Transfer Between Circular and Hyperbolic Orbits Using Analytical Maximum Thrust Arcs. Advances in the Astronautical Sciences. Vol.112. Part.II, 2002. pp. 671-689.

Azimov D.M., and Bishop H.R., Optimal Transfer Between Circular and Hyperbolic Orbits Using Analytical Maximum Thrust Arcs. AAS/AIAA Space Flight Mechanics Meeting. pp.1-20. Paper AAS 02-155. San Antonio, Texas. January 27-30, 2002.

Azimov D.M., and Bishop H.R, Planetary Capture Using Low -Thrust Propulsion. pp.1-31. Prepared for publication in the Journal of Spacecraft and Rockets.

Azimov, D.M., and Bishop, R.H., Turning Elliptical Orbital Planes via Intermediate Thrust Spherical Arcs. Journal of Spacecraft and Rockets. AIAA. 2002. Vol.25, N.2, pp.358-367.