DETERMINATION OF THE ATTITUDE OF THE SKYLARK ROCKET FROM A CONICAL SCANNING SUN-SLIT AND MAGNETOMETERS.
Abstract
The Memorandum describes the determination of the attitude of the Skylark rocket, using a conical scanning sun-slit and an orthogonal array of magnetometers, at the time of a pulse from the sun-slit. There are two attitudes which satisfy the data. The correct solution must be chosen by appealing to other information e.g. continuity of the attitude motion. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1968
- Accession Number
- AD0701474
Entities
People
- P. J. Herbert
Organizations
- Royal Aircraft Establishment