Closed loop simulation of optimum guidance of space vehicles by means of analogue computer techniques
- Paper ID
IAF-65-39
- author
- company
Dynamics Analysis and System studies, European Space Vehicle Launcher, Development Organisation
- country
France
- year
1965
- abstract
Analogue computers are the usual medium for simulating the dynamic behaviour of a missile, while trajectory calculation and guidance law evaluation are normally done on digital computers. In this report, an analogue method for simulating the movement of the centre of gravity will be given and three methods for simulating optimum guidance laws by parallel or sequential analogue techniques will be described.