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Vol 23, No 3 (2024)

Intelligent robust controllers for tribotronic conical fluid film bearings

Kazakov Y.N., Shutin D.V., Savin L.A.

(Rus)

Vol 20, No 1 (2021)

Algorithm for solving optimal open-loop terminal control problem for spacecraft rendezvous with account of constraints on the state

Shorikov A.F., Goranov A.Y.

(Rus)

Vol 23, No 1 (2024)

Optimization of trajectory motion of the first stage of an aerospace system

Khramov A.A.

(Rus)

Vol 22, No 2 (2023)

Controlled vibration protection systems: optimization and energy efficiency

Chernyshev V.I., Polyakov R.N., Fominova O.V.

(Rus)

Vol 18, No 3 (2019)

Disturbed motion of the hypersonic first stage of an aerospace system in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 18, No 2 (2019)

Disturbed motion of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

The automated control system of form of nonrigid shafts in lathing

Nabilkin A.U., Kravchenko S.A., Birukov V.P.

(Rus)

Vol 18, No 1 (2019)

Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle

Khramov A.A.

(Rus)

Vol 21, No 3 (2022)

Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere

Lyubimov V.V., Bakry I.

(Rus)

Vol 17, No 4 (2018)

Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust

Ishkov S.A., Filippov G.A., Fadeenkov P.V.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 9, No 2 (2010): Special Issue

Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust

1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 17, No 2 (2018)

Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 8, No 4 (2009)

Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis

Blinov A.O., Gurman V.I., Fralenko V.P.

(Rus)

Vol 19, No 3 (2020)

Disturbed transatmospheric motion of the first stage of an aerospace system

Krikunov M.M.

(Rus)

Vol 17, No 1 (2018)

Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 7, No 1 (2008)

System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization

Starinova O.L.

(Rus)

Vol 18, No 4 (2019)

Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver

Elisov N.A., Ishkov S.A., Khramov A.A.

(Rus)

Vol 16, No 3 (2017)

Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 7, No 1 (2008)

Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II

Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.

(Rus)

1 - 20 of 20 Items

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