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On the problem of optimal control of the thrust value of the electric propulsion rocket with solar energy source |
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| Institution: | 1. S.P. Timoshenko Institute of Mechanics NAS of Ukraine, 3, Nesterov St, 03057 Kyiv, Ukraine;2. National Taras Shevchenko University of Kyiv, 64, Volodymyrska St, 01033 Kyiv, Ukraine;1. PG Student, Civil Engineering Department, SardarVallabhbhai Patel Institute Of Technology, Vasad, 388306, India;2. Professor and Head, Civil Engineering Department, SardarVallabhbhai Patel Institute Of Technology, Vasad, 388306, India;2. School of Mechanical Engineering, Anhui Polytechnic University, Wuhu, 241000, PR China |
| Abstract: | Under consideration is the optimal control problem on a spacecraft motion in Newtonian central gravity field. With the use of the mathematical model of electrojet propulsion device (EPD) with solar energy source, proposed earlier in paper 1], the dependence of the EPD working substance choice on both the duration of the given dynamic maneuver and the propellant expenditures for its fulfillment is investigated. The efficiency evaluation is carrying out of optimal control of variable valued thrust as well as that for relay mode thrust and relay mode thrust with optimal fixed thrust value. |
| Keywords: | Real electric rocket engine Optimal control of rocket thrust Low thrust orbit transfer |
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