Partial Integrated Guidance and Control Design for Hypersonic Vehicle in Dive Phase
Q.K. Liu, J. Chen, L.X. Wang
Available Online May 2017.
- https://doi.org/10.2991/icmeit-17.2017.16How to use a DOI?
- Hypersonic vehicle, dive phase, terminal sliding mode control, partial integrated guidance and control
- Considering the potential unstable problem using Euler angle, the quaternion is used to take its place in proposed method. What is more, A partial integrated guidance control (PIGC) model is derived based on six-degree-freedom model to solve the guidance and control problems of hypersonic vehicle in dive phase, the desired body rates is calculated in the outer loop as virtual control signals by making use of the information of the state of vehicle and the relative motion between vehicle and target, and the fin deflection signals is obtained in inner loop by using the sliding mode controller to track the body rate commands. And the results of the simulation demonstrate the effectiveness of the proposed method.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Q.K. Liu AU - J. Chen AU - L.X. Wang PY - 2017/05 DA - 2017/05 TI - Partial Integrated Guidance and Control Design for Hypersonic Vehicle in Dive Phase BT - Proceedings of the 2nd International Conference on Mechatronics Engineering and Information Technology (ICMEIT 2017) PB - Atlantis Press SP - 81 EP - 88 SN - 2352-538X UR - https://doi.org/10.2991/icmeit-17.2017.16 DO - https://doi.org/10.2991/icmeit-17.2017.16 ID - Liu2017/05 ER -