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- [5] STABILITY DERIVATIVES FOR A SLENDER MISSILE WITH APPLICATION TO A WING-BODY-VERTICAL-TAIL CONFIGURATION JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (05): : 297 - 308
- [8] STABILITY OF THE UNIFORM ROTATION OF A GYROSTAT ROUND THE VERTICAL MAIN AXIS ON AN ABSOLUTELY SMOOTH HORIZONTAL PLANE PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1986, 50 (01): : 51 - 58