Design Methodology and Performance Evaluation of New Generation Sounding Rockets

Figure 13

Control law, attitude angles, and dynamic pressure in the thrust arc for the configuration with l = 7.29 m and d = 0.36 m (near radial guidance).

(a) In-plane control angle

(b) Out-of-plane control angle

(c) Roll angle

(d) Pitch angle

(e) Yaw angle

(f) Dynamic pressure constraint