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Title
Authors
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Creation of infotainment support of designing of control algorithms logic of spacecraft onboard control complexeses
1 1.
Computational algorithm of forming program motion in a scheduled turn of small spacecraft
Salmin V.V., Filatov A.V., Tkachenko I.S., Tyugashev A.A., Sopchenko E.V.
Development of information support for the spacecraft controlalgorithm design process
1 1., 1 1.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Method of improving control using a simulation object model and its application to the problem of helicopter emergency landing manoeuvre optimization
Kvokov V.N., Trushkova Y.A., Ukhin M.Y.
Usage of the graphical languages in lifecycle of embedded software for spacecrafts
1 1., 1 1.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
Visual approach to verifictaion of real-time control software
Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Control of the aircraft hydraulic system technical conditions on the basis of monitoring viscidity values and purity level of fluid power
Kovalev M.A., Borodkin G.V.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping
Onushkin Y.P., Sizov D.A., Poluyakhtov V.A., Ostrovoy A.V.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
Elisov N.A., Ishkov S.A., Khramov A.A.
Mathematical models of optimal investment control in fixed assets
Pavlov O.V., Moshkova T.A.
1 - 19 of 19 Items

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