Fixed-Time Sliding Mode Control for a Reusable Launch Vehicle in Attitude Adjustment Phase Including Actuator Dynamics
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-1099-7_22
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3. Baiocco, P.: Overview of reusable space systems with a look to technology aspects. Acta Astronaut. 189, 10–25 (2021)
4. Song, Z., Wang, C.: Powered soft landing guidance method for launchers with non-cluster configured engines. Acta Astronaut. 189, 379–390 (2021)
5. Sarkar, R., Amrr, S.M., Bhutto, J.K., Saidi, A.S., Algethami, A., Banerjee, A.: Finite time fractional order ISMC with time delay estimation for re-entry phase of RLV with enhanced chattering suppression. Acta Astronaut. 202, 130–138 (2023)
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