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Attitude control algorithms for a descent vehicle returning from the moon
- Source :
- Journal of Computer and Systems Sciences International. 56:483-491
- Publication Year :
- 2017
- Publisher :
- Pleiades Publishing Ltd, 2017.
-
Abstract
- We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing accuracy and an allowable load factor under the influence of a set of disturbances. Using the method of mathematical simulation, it is shown that the fuel consumption is reduced by ~30% in comparison with the initial stabilization parameters for the descent from a near-Earth orbit.
- Subjects :
- 010504 meteorology & atmospheric sciences
Computer Networks and Communications
Computer science
01 natural sciences
Physics::Geophysics
Theoretical Computer Science
Attitude control
0103 physical sciences
010303 astronomy & astrophysics
0105 earth and related environmental sciences
business.industry
Applied Mathematics
Numerical analysis
Deadband
Robotics
Load factor
Control and Systems Engineering
Fuel efficiency
Orbit (dynamics)
Astrophysics::Earth and Planetary Astrophysics
Computer Vision and Pattern Recognition
Artificial intelligence
Descent (aeronautics)
business
Algorithm
Software
Information Systems
Subjects
Details
- ISSN :
- 15556530 and 10642307
- Volume :
- 56
- Database :
- OpenAIRE
- Journal :
- Journal of Computer and Systems Sciences International
- Accession number :
- edsair.doi...........815f9acaa8f36d28476a98d2426eca74