Attitude control of an electrically propelled spacecraft utilizing the primary thrust system.
Computer simulated physical characteristics of electrically propelled spacecraft for selecting and designing attitude control system
Mankovitz, R. J.↗
Engineering topics
Mankovitz, R. J.
Publications and source records attributed to Mankovitz, R. J..
Computer program simulates physical systems by solving the simultaneous differential equations describing the systems
DIANA, a digital-analog simulation program for IBM 1620 2 computer, simulates physical systems by solving the simultaneous differential equations describing the systems. It expands and optimizes the input-output capabilities, permits additional flexibility in midstream program alternation, and minimizes the computational time.
Mankovitz, R. J.↗
The Analysis and Configuration of a Control System for a Mars Propulsive Lander
Analysis and configuration of control system for Mars propulsive lander
PLANETARY LANDING↗
Circuit exhibits power efficiency greater than 75 percent
Variable duty cycle pulser increases circuit power efficiency by more than 75 percent when operating solenoid valves. The pulser provides a low-level holding current after a high-level current has actuated the solenoid valves.
Mankovitz, R. J.↗
Guidance-and-control system sterilization
Sterilization of guidance and control systems and components
STERILIZATION↗