{
  "$type": "site.standard.document",
  "description": "A method for directly planning a reentry trajectory in a height-velocity profile includes the following steps: S, extracting an actual working parameter of an aircraft, setting the maximum value {dot over (Q)}of a stagnation point heat flux, the maximum value qof dynamic pressure, and the maximum…",
  "path": "/patents/1291861",
  "publishedAt": "2021-06-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C21/20",
    "DALIAN UNIVERSITY OF TECHNOLOGY"
  ],
  "textContent": "A method for directly planning a reentry trajectory in a height-velocity profile includes the following steps: S, extracting an actual working parameter of an aircraft, setting the maximum value {dot over (Q)}of a stagnation point heat flux, the maximum value qof dynamic pressure, and the maximum value nof overload according to the mission requirement, and solving the height-velocity boundary of the reentry trajectory, that is, a lower boundary of the reentry trajectory in the height-velocity profile; S, solving a reentry trajectory of an initial descent stage according to differential equations of reentry motion, and determining a starting point of a trajectory of a gliding stage according to the trajectory of the initial descent stage; and S, planning a trajectory in the height-velocity profile satisfying terminal constraints based on the lower boundary in the height-velocity profile, and calculating a corresponding bank angle, to obtain the reentry trajectory.",
  "title": "METHOD FOR DIRECTLY PLANNING REENTRY TRAJECTORY IN HEIGHT-VELOCITY PROFILE"
}