公开(公告)号：US10281890B1

公开(公告)日：2019-05-07

申请号：US16126062

申请日：2018-09-10

申请人： Kitty Hawk Corporation

发明人： Ilan Kroo ,  Marshall Gusman ,  Neel Vora ,  Jim Bungener ,  Eric Allison

IPC分类号： G05B17/02 ,  B64C39/02 ,  G05D1/08 ,  B64C27/22

摘要： A flight control system is disclosed. In various embodiments, a flight control system includes a data storage device configured to store an aerodynamic model; and a processor coupled to the data storage device and configured to use the aerodynamic model to determine a set of actuators and for each actuator in the set a corresponding set of one or more actuator parameters to achieve a desired set of forces and moments. The aerodynamic model provides for each actuator in the set of actuator corresponding force and moment data for each of a first set of operating conditions based on a first set of simulations performed by varying one or more actuator parameters while holding other actuators at a baseline value and a second set of simulations to determine interactions between the actuator and said other actuators under each of a second set of operating conditions.

公开(公告)号：US10101719B1

公开(公告)日：2018-10-16

申请号：US15838790

申请日：2017-12-12

申请人： Kitty Hawk Corporation

发明人： Ilan Kroo ,  Marshall Gusman ,  Neel Vora ,  Jim Bungener ,  Eric Allison

IPC分类号： G05B17/02 ,  B64C39/02 ,  G05D1/08 ,  B64C27/22

摘要： A flight control system is disclosed. In various embodiments, a flight control system includes a data storage device configured to store an aerodynamic model; and a processor coupled to the data storage device and configured to use the aerodynamic model to determine a set of actuators and for each actuator in the set a corresponding set of one or more actuator parameters to achieve a desired set of forces and moments. The aerodynamic model provides for each actuator in the set of actuator corresponding force and moment data for each of a first set of operating conditions based on a first set of simulations performed by varying one or more actuator parameters while holding other actuators at a baseline value and a second set of simulations to determine interactions between the actuator and said other actuators under each of a second set of operating conditions.