2020.01.16向峻宏
这个代码还是挺难懂的,因为他的那个三部分的飞机模型的理论知识我没学过,如果能了解到它的运行原理,对于代码理解要好很多,如果哪位同学有四旋翼无人机的原理知识,就告诉我一下吧!
include "Quadrotor.h"
include "utils.h"
include <Eigen/Geometry>
Quadrotor::Quadrotor()
{
physics = RigidBody();
prop_radius = 0.099;
kf = 5.55e-8;
km = 0.07*(2*prop_radius)*kf;
arm_length = 0.17;
motor_time_constant = 1.0/20;
min_rpm = 1200;
max_rpm = 7000;/*定义了旋翼半径,桨叶推力系数kf,桨叶时间系数km(不懂啥意思,从下面的代码推出来的),旋翼机臂长,动机持续时间,最大和最小转速*/
type = QUAD_MOTOR_CROSS;/*旋翼类型,就是下面的图展示的*/
/* bug record: does not initialize here */
external_force = Eigen::Vector3d::Zero();
external_torque = Eigen::Vector3d::Zero();/*这好像是刚体的力和转矩,函数名和刚体里面的代码名一样*/
}
void Quadrotor::sim_step(double dt)/*四旋翼仿真的一步*/
{
Eigen::Array4d motor_rpm_dot;
Eigen::Array4d motor_rpm_sq = motor_rpm.array().square();
double thrust = kf*motor_rpm_sq.sum();/*旋翼的推力计算公式*/
Eigen::Vector3d force;
Eigen::Vector3d torque;
Eigen::Quaterniond my_attitude = physics.get_attitude();
/* different torque if we have different type of quadrotor */
if (type == QUAD_MOTOR_CROSS)
{
/*
1
|
|
2 ----------- 3
|
|
0
*/
torque(0) = kf*(motor_rpm_sq(2) - motor_rpm_sq(3))*arm_length;
torque(1) = kf*(motor_rpm_sq(1) - motor_rpm_sq(0))*arm_length;
torque(2) = km*(motor_rpm_sq(0) + motor_rpm_sq(1) -
motor_rpm_sq(2) - motor_rpm_sq(3));/*计算三个转矩,前2个是当前平面内的x,y轴的转矩,第三个我没懂*/
}
//TODO:add QUAD_MOTOR_X
/*
1 0
\ /
\ /
\ /
/ \
/ \
/ \
2 3
*/
force = my_attitude.toRotationMatrix().col(2)*thrust + external_force;
/* only for debug */
//force = thrust*Eigen::Vector3d::UnitZ() + external_force;
torque = torque + external_torque;/*计算总的力和转矩*/
/* physics simulation */
physics.set_force(force);
physics.set_torque(torque);
physics.sim_step(dt);/*刚体rigid body进行仿真的一步*/
motor_rpm_dot = (target_motor_rpm - motor_rpm)/motor_time_constant;/*单位时间要增加的动机转速*/
motor_rpm += motor_rpm_dot*dt;/*动机转速调整*/
}
void Quadrotor::set_motor_rpms(double m1, double m2, double m3, double m4)
{
target_motor_rpm(0) = double_limit(m1, min_rpm, max_rpm);
target_motor_rpm(1) = double_limit(m2, min_rpm, max_rpm);
target_motor_rpm(2) = double_limit(m3, min_rpm, max_rpm);
target_motor_rpm(3) = double_limit(m4, min_rpm, max_rpm);/*设置四个动机转速*/
}
void Quadrotor::set_external_force(Eigen::Vector3d _force)
{
external_force(0) = _force(0);
external_force(1) = _force(1);
external_force(2) = _force(2);/*设置三个外力*/
}
void Quadrotor::set_external_torque(Eigen::Vector3d _torque)
{
external_torque(0) = _torque(0);
external_torque(1) = _torque(1);
external_torque(2) = _torque(2);/*设置三个外部转矩*/
}
Eigen::Quaterniond Quadrotor::get_attitude()
{
return physics.get_attitude();/*这里应该是调用刚体的姿态函数获取刚体的姿态*/
}
void Quadrotor::set_attitude(Eigen::Quaterniond _attitude)
{
physics.set_attitude(_attitude);/*设置目标姿态*/
}
Eigen::Vector3d Quadrotor::get_position()
{
return physics.get_position();/*获取位置信息*/
}
void Quadrotor::set_position(Eigen::Vector3d setting_vec)
{
physics.external_set_position(setting_vec);/*设置目标位置*/
}
Eigen::Vector3d Quadrotor::get_velocity()
{
return physics.get_velocity();/*获取速度,以下类推*/
}
double Quadrotor::get_mass()
{
return physics.get_mass();
}
Eigen::Vector3d Quadrotor::get_angularVelocity() const
{
return physics.get_angularVelocity();
}
Eigen::Matrix3d Quadrotor::get_inertia() const
{
return physics.get_inertia();
}
double Quadrotor::get_propeller_thrust_coefficient(void) const
{
return kf;
}
double Quadrotor::get_propeller_moment_coefficient(void) const
{
return km;
}
double Quadrotor::get_arm_length(void) const
{
return arm_length;
}
QUAD_MOTOR_TYPE Quadrotor::get_type(void) const
{
return type;
}