Instrumental realization of a controlling lambda-mu functional, not requiring an integrating computer
Abstract
Il'shinskii (1968) has proposed a method for determining the control lambda-mu functional on board a spacecraft from the readings of two apparent-acceleration integrators, the running readings of the integrator with the sensitive axis oriented in the mu-direction (mu-integrator) being integrated on an onboard computer. In the present paper, it is shown that the use of the computer can be eliminated, provided the acceleration integrators are of gyroscopic type.
- Publication:
-
Prikladnaia Mekhanika
- Pub Date:
- December 1976
- Bibcode:
- 1976PriM...12..120K
- Keywords:
-
- Functionals;
- Gyroscopes;
- Spacecraft Control;
- Spacecraft Guidance;
- Airborne/Spaceborne Computers;
- Block Diagrams;
- Integrators;
- Missile Control;
- Space Communications, Spacecraft Communications, Command and Tracking