| Paper Code | Title | Authors | Topic |
|---|
| Fr-A18-TO/1 | New Guidance Law and Autopilot Design for Launch Rockets | Cheng Chia-Hao, Yeh Fu-Kuang, Fu Li-Chen | 7.3 |
| Fr-A18-TO/2 | Attitude Control of Flexible Launch Vehicle Using Adaptive Notch Filter | Oh Choong-Seok, Bang Hyochoong | 7.3 |
| Fr-A18-TO/3 | LQG Controller Designs from Reduced Order Models for a Launch Vehicle | Dhabale Ashwin, Banavar Ravi, Dhekane M. V. | 7.3 |
| Fr-A18-TO/4 | Missile Autopilot Controlled by Aerodynamic Lift and Divert Thrusters via Second-order Sliding Mode | Shtessel Yuri, Tournes Christian, Shkolnikov Ilya | 7.3 |
| Fr-A18-TO/5 | Autopilot Design for Agile Missile Using LTV Control and Nonlinear Dynamic Inversion | Choi Jae Weon, Lee Ho Chul | 7.3 |
| Fr-A18-TO/6 | Input-Dependent Threshold Function fo an Actuator Fault Detection Filter | Rotstein Hector, Ingvalson Ryan, Keviczky Tamas, Balas Gary | 7.3 |
