公开(公告)号：US20130306787A1

公开(公告)日：2013-11-21

申请号：US13778212

申请日：2013-02-27

Applicant: Prox Dynamics AS

Inventor： Trygve Frederik Marton ,  Geir Morten Egeberg Mellem ,  Pal Hagh Sandberg ,  Petter Muren ,  Dag Henning Paulsen

IPC: B64C19/00

CPC classification number: B64C19/00 ,  B64C27/04 ,  B64C27/57 ,  G05D1/0858

Abstract: A method and device for precise control of and controller design for aircrafts consisting of at least one spinning part and at least one non spinning part is provided. The required torques for control of the spinning parts and for the non-spinning parts are continuously and individually calculated. All torques are combined to get the correct torque for the complete aircraft. Doing this, it's possible to continuously apply the correct torque, both correctly distributed among the roll and pitch axes (correct angle), and correct magnitude. The result is a decoupling of the roll and pitch axes, simplifying controller design to a design of two single input single output controllers, one for each axe.

Abstract translation: 提供了由至少一个纺纱部分和至少一个非纺纱部分组成的用于飞机的精确控制和控制器设计的方法和装置。 用于控制纺纱部件和非纺纱部件的所需扭矩是连续和单独计算的。 所有扭矩相结合，以获得整个飞机的正确扭矩。 做到这一点，可以连续地应用正确分配在滚动轴和俯仰轴之间的正确扭矩（正确的角度），并确定大小。 结果是滚动和俯仰轴的解耦，简化了控制器设计到两个单输入单输出控制器的设计，每个轴一个。

公开(公告)号：US08682506B2

公开(公告)日：2014-03-25

申请号：US13778212

申请日：2013-02-27

Applicant: Prox Dynamics AS

Inventor： Trygve Frederik Marton ,  Geir Morten Egeberg Mellem ,  Pal Hagh Sandberg ,  Petter Muren ,  Dag Henning Paulsen

IPC: G05D1/08 ,  B64C27/467

CPC classification number: B64C19/00 ,  B64C27/04 ,  B64C27/57 ,  G05D1/0858

Abstract: A method and device for precise control of and controller design for aircrafts consisting of at least one spinning part and at least one non-spinning part is provided. The required torques for control of the spinning parts and for the non-spinning parts are continuously and individually calculated. All torques are combined to get the correct torque for the complete aircraft. Doing this, it's possible to continuously apply the correct torque, both correctly distributed among the roll and pitch axes (correct angle), and correct magnitude. The result is a decoupling of the roll and pitch axes, simplifying controller design to a design of two single input single output controllers, one for each axe.

Abstract translation: 提供了由至少一个纺纱部分和至少一个非纺纱部分组成的用于飞机的精确控制和控制器设计的方法和装置。 用于控制纺纱部件和非纺纱部件的所需扭矩是连续和单独计算的。 所有扭矩相结合，以获得整个飞机的正确扭矩。 做到这一点，可以连续地应用正确分配在滚动轴和俯仰轴之间的正确扭矩（正确的角度），并确定大小。 结果是滚动和俯仰轴的解耦，简化了控制器设计到两个单输入单输出控制器的设计，每个轴一个。