This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
A Control Scheme for Attitude Control of Large Flexible Boosters
Annotation ability available
Sector:
Language:
English
Abstract
Authors
Topic
Citation
Kopp, R. and White, R., "A Control Scheme for Attitude Control of Large Flexible Boosters," SAE Technical Paper 610115, 1961, https://doi.org/10.4271/610115.Also In
References
- Geissler E. D. “Problems in Attitude Stabilization of Large Guided Missiles.” Aerospace Engineering Oct 1960
- Smith G. W. “Synthesis of a Self Adaptive Autopilot for a Large Elastic Booster” IRE Trans. on Automatic Control AC-5 3 Aug 1960
- Smyth R. K. DuPlessis R. M. Mattingly L. K. “A Digital Self-Adaptive Body Bending Filter for Flexible Airframe Control.” Autonetics Div. of North American Aviation, Inc. Nov 1960
- Lukens D. R. “Methods of Analysis of a Control System for a Large Flexible Missile.” National Specialists Meeting on Aerospace Vehicles Boston May 1960
- Kachigan K. “The General Theory and Analysis of a Flexible Bodied Missile with Autopilot Control.” USAF Contract No. AF 04(645) -4, Convair Report No. ZU-7.048 Nov 1955