A STUDY OF AN ATTITUDE CONTROL SYSTEM FOR THE BLACK ARROW LAUNCHING VEHICLE.
Abstract
A specification for the Black Arrow attitude control system during the coasting phase is outlined. Consideration is given to the choice of system and the total impulse required, and it is concluded that reaction jets should be used with stored gaseous nitrogen or air as propellent. The performance of such a system during acquisition and limit cycle motion is analysed using phase-plane techniques with emphasis on the effects of valve delays, and the results of an analogue simulator study are recorded. Various methods of generating a signal proportional to angular rate are considered and the use of a rate gyro is tentatively recommended. Some engineering aspects of the design are examined including the choice of the control valve. Recommendations are made concerning testing philosophy and the development programme. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1965
- Accession Number
- AD0634207
Entities
People
- C. H. Garnett
- R. G. Langton
Organizations
- Royal Aircraft Establishment