Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stage
Gimbaled nozzle and liquid injection thrust vector control requirements for solid rocket two stage launch vehicles
Borsody, J.↗
Engineering topics
Scalzott, L. L.
Publications and source records attributed to Scalzott, L. L..
Digital simulation stability criterion.
Digital simulation computer stability analysis scheme premised on use of perturbed transient responses
Lorenzo, C. F.↗
Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements
Load relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds
Scalzott, L. L.↗
Computer program determines system stability /DIGSTA/
Computer program implements a stability criterion that can be applied directly to the numerical solutions of systems of differential equations. The program accepts as input the time function of the system, a time to view the transient, and an acceptable amplitude boundary for any steady-state oscillation.
Lorenzo, C. F.↗
Practical stability criterion and its application to digital simulation
Stability criterion for digital simulation
Lorenzo, C. F.↗