Motivation for research in stability theory
Analytical methods to determine capability of space vehicle guidance system, and Liapunov functions for stability of nonlinear systems
Dearman, C. C., Jr.↗
Engineering topics
Publications and source records attributed to Dearman, C. C., Jr..
Analytical methods to determine capability of space vehicle guidance system, and Liapunov functions for stability of nonlinear systems
Artificial earth satellite orbital elements first order secular perturbations due to sun and moon mass derived, using Lagrangian perturbation equations
Liapunov functions generating methods applicable to nonlinear and linear autonomous systems