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- W2331519079 abstract "Under prospect of realizing fully reusable launch vehicle, authors have proposed an Aerospace plane /EkeranopLane system concept[l][2][3]. The Aerospace plane/Ekranoplane system concept consists of a reusable winged launch vehicle and an Ekranoplane. Ekranoplane is a huge wing in groundeffect (WIG) craft which can move with a velocity of more than 0.5 M several meters high above sea level, carrying heavy payloads. Aerospace plane (ASP) will be launched and landed horizontally using Ekranoplane as a takeoff and landing assist. Ekranoplane with its own mass of 1500 tons has a capability of launching ASP with starting mass of about 600 tons from any point on the sea. Another advantageous feature of this system is an opportunity for ASP to land on moving Ekranoplane at the final phase of the recovery from the orbit. The landing concept consists in docking ASP with Ekranoplane, which consequently requires no undercarriage and runway. There are two major problems at landing of aerospace plane on Ekranoplane, approaching and docking. Both of them have to be solved with high reliability and accuracy. This paper discusses about the landing variants and principles of motion control laws optimization." @default.
- W2331519079 created "2016-06-24" @default.
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- W2331519079 date "1998-01-12" @default.
- W2331519079 modified "2023-09-27" @default.
- W2331519079 title "Optimization of motion control at landing of aerospace plane on Ekranoplane" @default.
- W2331519079 cites W2727381586 @default.
- W2331519079 doi "https://doi.org/10.2514/6.1998-305" @default.
- W2331519079 hasPublicationYear "1998" @default.
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