DocumentCode :
2107202
Title :
Concept and advantages of spaceplane water landing with ekranoplane assist
Author :
Nebylov, Alexander ; Tomita, Nobuyuki
Author_Institution :
Int. Inst. for Adv. Aerosp. Technol., State Univ. of Aerosp. Instrum., St. Petersburg, Russia
fYear :
2005
fDate :
24-26 Aug. 2005
Firstpage :
485
Lastpage :
490
Abstract :
The concept of spaceplane landing with ekranoplane assist is developed. It is shown, that realizability of their docking at a final stage of spaceplane alighting gives hopeful prospect for expansion of functional capacity of aerospace transport system. The possible versions of spaceplane landing without application of wheeled gear are described. The requirements to applicable automatic systems of motion control of both winged vehicles are discussed. Some physical approached for navigation devises and integrated system of relative motion control design are suggested.
Keywords :
aerospace control; aerospace safety; aircraft landing guidance; motion control; space vehicles; aerospace transport system; automatic system; docking; ekranoplane; flight control; integrated system; motion control; navigation devises; spaceplane alighting; spaceplane water landing; wheeled gear; winged vehicle; Aerospace electronics; Costs; Gears; Motion control; Motion planning; Payloads; Sea surface; Space technology; Space vehicles; Transportation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Physics and Control, 2005. Proceedings. 2005 International Conference
Print_ISBN :
0-7803-9235-3
Type :
conf
DOI :
10.1109/PHYCON.2005.1514032
Filename :
1514032
Link To Document :
بازگشت