Paper information

Paper code

IAC-17,D2,6,9,x39260

Order

9

Room

Hall O

Title

the modeling and terminal sliding mode fine attitude control for aeroelastic hypersonic vehicle

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-17

Type of presentation

oral

Main author

Dr. Jie Liang, China