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A NEW EFFICIENT METHOD TO BOUNDARY VALUE PROBLEM FOR BALLISTIC ROCKET GUIDANCE
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作者 刘新建 袁天保 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2005年第10期1375-1381,共7页
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 w... 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 performances of stability, robustness, high precision, and algebraic formulas in real computation. By virtue of modern DSP (digital signal processor ) high speed chip technology, the algorithm can be used in real time and can adaot to the requirements of the big primary bias of rocket guidance. 展开更多
关键词 rocket guidance and control bounoary value problem numerical iteration
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