3D Guidance Algorithm for TAEM Phase Based on Coupling Coefficient

Author:

Zhu Gaocan,Quan Shenming,Chao Tao,Wang Songyan

Publisher

Springer Singapore

Reference14 articles.

1. Gong, Y., Chen, S.: TAEM vertical profile optimization algorithm for reentry vehicle. Aerosp. Control Appl. 44(03), 28–35 (2018)

2. Mu, L., Li, P., Wang, X., Ma, T.: Trajectory planning and guidance for terminal area energy management phase of reusable launch vehicle. Aerosp. Control 36(01), 23–29 (2018)

3. Liu, Z., He, Y.: Composite guidance based on onboard trajectory generation for terminal area energy management. Tactical Missile Technol. (04), 66–72 (2017)

4. Mu, L., Li, P., Li, L., Wang, X., Xie, R.: Onboard trajectory planning algorithm for terminal area energy management phase of a RLV. Syst. Eng. Electron. 39(03), 591–598 (2017)

5. Dong, Q.: Trajectory Optimization and Attitude Tracking Control for Reusable Launch Vehicle, p. 130. TianjinUniversity (2017)

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