A New Efficient Method to the Boundary Value Problem for Ballistic Rocket Guidance

LIU Xin-jian; YUAN Tian-bao

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LIU Xin-jian, YUAN Tian-bao. A New Efficient Method to the Boundary Value Problem for Ballistic Rocket Guidance[J]. Applied Mathematics and Mechanics, 2005, 26(10): 1247-1252.

Citation:

LIU Xin-jian, YUAN Tian-bao. A New Efficient Method to the Boundary Value Problem for Ballistic Rocket Guidance[J]. Applied Mathematics and Mechanics, 2005, 26(10): 1247-1252.

Citation:

LIU Xin-jian, YUAN Tian-bao. A New Efficient Method to the Boundary Value Problem for Ballistic Rocket Guidance[J]. Applied Mathematics and Mechanics, 2005, 26(10): 1247-1252.

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A New Efficient Method to the Boundary Value Problem for Ballistic Rocket Guidance

Institute of Aerospace Engineering, National University of Defense Technology, Changsha 410073, P. R. China

Received Date: 2003-11-11
Rev Recd Date: 2005-03-15
Publish Date: 2005-10-15

Abstract

Abstract

The exploitation of rocket guidance technology on the basis of the guidance law of Space Shuttle and Pegasus rocket was performed. A new efficient method of numerical iteration solution to the boundary value problem was put forward. The numerical simulation results have shown that the method features good performance of stability, robustness, high precision, and algebraic formulas in real computation. By virtue of modern digital signal processor(DSP), high speed chip technology, the algorithm can be used in real time and can adapt to the requirements of the big primary bias of rocket guidance.
- rocket guidance and control,
- boundary value problem,
- numerical iteration

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References(8)

References

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