NUMERICAL INTEGRATION METHODS FOR BALLISTIC ROCKET TRAJECTORY SIMULATION PROGRAMS
ARMY ELECTRONICS COMMAND WHITE SANDS MISSILE RANGE NM ATMOSPHERIC SCIENCES LAB
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Numerical integration methods for solution of the system of differential equations found in ballistic rocket trajectory programs are discussed. The general discussion entails the explicit formulas of Runge-Kutta and predictor-corrector methods and their errors, and a brief description of other methods that could be employed.
- Theoretical Mathematics