Since the successful flights of Apollo capsule and Space Shuttle, researches on entry guidance algorithm have made impressive and remarkable progress.
Linear Pseudospectral Reentry Guidance with Adaptive Flight Phase Segmentation and Eliminating General Nominal Effort Miss Distance
Steady Glide Dynamics and Guidance of Hypersonic Vehicle ; Chapter : 16 ; 389-432
2020-11-08
44 pages
Article/Chapter (Book)
Electronic Resource
English
Linear Pseudospectral Guidance Method for Eliminating General Nominal Effort Miss Distance
Springer Verlag | 2020
|Minimum Effort Pursuit/Evasion Guidance with Specified Miss Distance
British Library Conference Proceedings | 2015
|Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method
Online Contents | 2011
|