Instantaneous Impact Point Guidance with Coast Arcs for Solid Rockets
This paper proposed an analytical iterative guidance method with the desired instantaneous impact point constraint for solid rockets in “burn-coast-burn” trajectory mode. Solid rocket motors expect to remove the thrust termination mechanism to increase the structural strength and launch reliability,...
Saved in:
Main Authors: | Shengwei Jia, Fugui Li, Mingbo Tong |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/5571877 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles
by: Si-Yuan Chen, et al.
Published: (2016-01-01) -
Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles
by: Shengwei Jia, et al.
Published: (2020-01-01) -
Damped Iterative Explicit Guidance for Multistage Rockets with Thrust Drop Faults
by: Zongzhan Ma, et al.
Published: (2025-01-01) -
Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework
by: Jingqi Li, et al.
Published: (2022-01-01) -
Modelling and Neuro-Adaptive Robust Control Algorithms for Solid Fuel Rockets
by: Christian Danner Ramos de Carvalho, et al.
Published: (2025-01-01)