GUIDANCE AND CONTROL DURING DIRECT-DESCENT PARABOLIC REENTRY
Abstract
Four guidance and control techniques applicable to the reentry from parabolic orbits of vehicles having low lift-drag ratios are described. Techniques include pilot and automatic control to a reference trajectory and the use of prediction to improve and simplify guidance procedures. Comparison between systems is made and areas where further study may be profitable are indicated.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1961
- Accession Number
- AD0266591
Entities
People
- Edwin C. Foudriat
- Rodney C. Wingrove
Organizations
- National Aeronautics and Space Administration