Optimal Terminal Guidance with Constraints at Final Time
- 1 June 1977
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 14 (6) , 381-383
- https://doi.org/10.2514/3.57212
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Velocity of bodies powered by diatomic cold-gas thrustersJournal of Spacecraft and Rockets, 1976
- Velocity of bodies powered by rapidly discharged cold-gas thrustersJournal of Spacecraft and Rockets, 1975
- Terminal Guidance for Impact Attitude Angle Constrained Flight TrajectoriesIEEE Transactions on Aerospace and Electronic Systems, 1973
- Discrete optimal terminal control with application to missile guidanceIEEE Transactions on Automatic Control, 1973
- Fundamentals of proportional navigationIEEE Spectrum, 1966
- Missile Guidance by Three-Dimensional Proportional NavigationJournal of Applied Physics, 1956