References
- D. S. Cartan, "Rocket Propulsion Technology", Plenum, 1961.
- 이용인, 조성진, 최동균, "비행제어를 위한 비행중 고체로켓 추력 예측 방법", 한국군사과학기술학회 종합학술대회, 경주, 2012.
DOI QR Code
In this paper, we propose a method of generating pitch commands for consistent initial trajectories irrelevant to flight conditions in the initial boosting phase of a thrust-vector-controlled vehicle. After shape assumption of the pitch command profile, parameters of the profile are determined in real time in order for the summit height of the trajectory to be a desired value by deriving the summit height considering thrust performance, gravity, and other flight conditions. Computer simulation results demonstrate good performance of the proposed method.