Translated by Z. Lerman. — Published for the National Aeronautics and Space Administration and the National Science Foundation, Washington, D.C. by the Israel Program for Scientific Translations, Jerusalem, 1969. — 426 p.
Перевод на английский язык книги Андреев В. Д. Теория инерциальной навигации (корректируемые системы), 1967 г.
Elements of the theory of autonomous inertial navigation systems
Aided inertial systems: Altimeter correction
Schuler-tuned gyropendulum systems. Analogy with two-accelerometer inertial systems
Simplified operation equations of ideal and perturbed two-accelerometer inertial systems
Inertial systems with Doppler correction
Astronomical correction of inertial navigation systems. Combined astro-Doppler correction
Dynamics of inertial systems with random instrumental errors
Appendix I. Scattered solar radiation in the atmosphere as an example of determinate errors in phase astrocorrection systems
Appendix II. Navigation using a directional gyroscope and a Doppler velocity meter
Appendix III. Accelerometer guidance
ELEXIENTS OF THE THEORY OF AUTOKOR-IOUS