Paper information

Paper code

IAC-16,D2,6,10,x33427

Order

10

Room

Salon Jalisco E2

Title

the application of attitude for high-order nonsingular terminal sliding mode control of dynamics model of hypersonic vehicle by differential linearized processing through channel of speed and height

abstract

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Session

6. Future Space Transportation Systems Verification and In-Flight Experimentation

symposium

D2. SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

congress

IAC-16

Type of presentation

oral

Main author

Dr. Jie Liang, China

Co-authors

Prof. Li Chen, Fuzhou University, China;