S.A. Reshmin, M.T. Bektybaeva. Effective control of the dynamics of a point object with a bounded thrust ... P. 203-220

The article is devoted to the problem of optimal control of an object performing a high-speed maneuver in a plane with bounded thrust under the influence of the external forces. The purpose is to maximize the velocity along a given line in a finite specified time. The linear tangent law is used as the optimal control law. As an analog, a relay suboptimal control with a simpler structure is developed, the choice of which is governed by theorems and hypotheses depending on the initial velocity and process time. Domains are constructed that cover the conditions of each theorem within the solvability conditions of the problem.

Keywords: optimal control, suboptimal control, linear tangent law, trajectory optimization, bounded thrust

Received February 16, 2026

Revised March 20, 2026

Accepted March 23, 2026

Funding Agency: The work was completed on the topic of the state assignment (state registration number 124012500443-0).

Sergey Aleksandrovich Reshmin, Dr. Phys.-Math. Sci., Corresponding Member of RAS, Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences, Moscow, 119526 Russia, e-mail: reshmin@ipmnet.ru

Madina Timurovna Bektybaeva, Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences, Moscow, 119526 Russia, e-mail: bektybaeva@ipmnet.ru

REFERENCES

1.   Isaev V.K. Pontryagins’s maximum principle and optimal programming of rocket thrust. Avtomat. i Telemekh., 1961, vol. 22, no. 8, pp. 986–1001 (in Russian).

2.   Levskii M.V. Optimal orientation control of a space vehicle with restrictions on the control and phase variables. J. Comput. Syst. Sci. Inter., 2021, vol. 60, iss. 6, pp. 1027–1045. https://doi.org/10.1134/S1064230721030096

3.   Kim Y., Cho N., Park J., Kim Y. Online trajectory replan for gliding vehicle considering terminal velocity constraint. IEEE Trans. Aerospace Electron. Syst., 2023, vol. 59, no. 2, pp. 1067–1083. https://doi.org/10.1109/TAES.2022.3197103

4.   Perkins F.M. Derivation of linear-tangent steering laws. Air Force Report No. SSD-TR66-211, Nov. 1966, 22 p. https://doi.org/10.21236/ad0643209

5.   Gordan A.L. Centaur D-1A guidance/software system. In: Proc. Conf. “Annual Rocky Mountain Guidance and Control Conference”, Keystone, Colorado, 1984, 17 p.

6.   Brusch R.G. Bilinear tangent yaw guidance. In: Proc. Conf. “Guidance and Control”, Boulder, Colo., 1979, pp. 250–264.

7.   Kim K.S., Park J.W., Tahk M.J., Choi H.L. A PEG-based ascending guidance algorithm for ramjet-powered vehicles. In: Proc. 28th Inter. Congress of the Aeronautical Sciences (ISAC 2012), 2012, 7 p.

8.   Lugo R.A., Shidner J.D., Powell R.W., Marsh S.M., Hoffman J.A., Litton D.K., Schmitt T.L. Launch vehicle ascent trajectory simulation using the program to optimize simulated trajectories II (POST2). In: Proc. Conf. AAS/AIAA Space Flight Mechanics Meeting, no. NF1676L-25552, February, 2017, 13 p.

9.   Reshmin S.A. Optimal traction control in high-speed maneuvering under dry friction conditions. Mech. Solids, 2023, vol. 58, no. 7, pp. 2574–2585. https://doi.org/10.3103/S0025654423070191

10.   Bektybaeva M.T., Reshmin S.A. Efficient control of the direction of thrust during high-speed maneuver in the plane. Vestnik Ross. Univ. Druzhby Narodov, Ser. Ingener. Issled., 2023, vol. 24, no. 3, pp. 233–240 (in Russian). https://doi.org/10.22363/2312-8143-2023-24-3-233-240

11.   Bryson A.E., Ho Y.-C. Applied optimal control: optimization, estimation, and control. Waltham, Mass., Blaisdell Pub. Co., 1969, 481 p. Translated to Russian under the title Prikladnaya teoriya optimal’nogo upravleniya, Moscow, Mir Publ., 1972, 544 p.

12.   Pontryagin L.S., Boltyanskii V.G., Gamkrelidze R.V., Mishchenko E.F. The mathematical theory of optimal processes, NY, London, Sydney, John Wiley & Sons, 1962, 360 p. ISBN-13: 978-0470693810 . Original Russian text published in Matematicheskaya teoriya optimal’nykh protsessov, Moscow, Nauka Publ., 1983, 392 p.

13.   Reshmin S.A., Bektybaeva M.T. Control of acceleration of a dynamic object by the modified linear tangent law in the presence of a state constraint. Proc. Steklov Inst. Math. (Suppl. iss.), 2024, vol. 325, iss. 1, pp. S168–S178. https://doi.org/10.1134/S0081543824030131

Cite this article as: S.A. Reshmin, M.T. Bektybaeva. Effective control of the dynamics of a point object with a bounded thrust. Trudy Instituta Matematiki i Mekhaniki UrO RAN, 2026, vol. 32, no. 2, pp. 203–220.