Referring to FIG. 2, a particular diagram of the system 200 that is operable to dynamically modify an initial trajectory profile during flight is shown. The system 200 includes a flight management system 202 (e.g., a controller), a memory 204 coupled to the flight management system 202, an input interface 206 coupled to the flight management system 202, a flight condition monitor 208 coupled to the flight management system 202, a display screen 210 coupled to the flight management system 202, and one or more systems 290 coupled to the flight management system 202. The one or more systems 290 include an autopilot system 292. According to some implementations, one or more components of the system 200 are integrated into the flight management system 202. As a non-limiting example, the input interface 206 and the flight condition monitor 208 can be integrated into the flight management system 202.
