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bf_original_balance_chassis/application/chassis/lqr_calc.h

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#include "balance.h"
#include "stdint.h"
#include "arm_math.h"
/**
* @brief ,LQR的反馈增益,LQR的输出
* @note
*
*/
static void CalcLQR(LinkNPodParam *p, ChassisParam *chassis)
{
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static float k[12][3] = {91.443258,-113.149301,-8.780431,
2.186397,-6.908826,-0.171192,
47.943203,-39.423913,-13.297140,
30.671413,-28.308799,-9.363969,
231.778706,-224.742110,68.974495,
18.910995,-20.079072,7.490403,
50.114072,-58.670210,23.856863,
3.273746,-3.321150,1.267603,
140.969395,-137.481822,42.507159,
93.859327,-90.754295,27.811839,
-283.581279,232.017305,87.865897,
-28.193619,23.802666,3.963794,};
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float T[2] = {0}; // 0 T_wheel 1 T_hip
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float l = p->leg_len;
float lsqr = l * l;
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uint8_t i, j;
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// 离地时轮子输出置0
i = 0; j = i * 6;
T[i] = p->fly_flag ? 0 :
((k[j + 0][0] * lsqr + k[j + 0][1] * l + k[j + 0][2]) * -p->theta +
(k[j + 1][0] * lsqr + k[j + 1][1] * l + k[j + 1][2]) * -p->theta_w +
(k[j + 2][0] * lsqr + k[j + 2][1] * l + k[j + 2][2]) * (chassis->target_dist - chassis->dist) +
(k[j + 3][0] * lsqr + k[j + 3][1] * l + k[j + 3][2]) * (chassis->target_v - chassis->vel) +
(k[j + 4][0] * lsqr + k[j + 4][1] * l + k[j + 4][2]) * -chassis->pitch +
(k[j + 5][0] * lsqr + k[j + 5][1] * l + k[j + 5][2]) * -chassis->pitch_w);
// 离地时关节输出仅保留 theta 和 theta_dot保证滞空时腿部竖直
i = 1; j = i * 6;
T[i] = (k[j + 0][0] * lsqr + k[j + 0][1] * l + k[j + 0][2]) * -p->theta +
(k[j + 1][0] * lsqr + k[j + 1][1] * l + k[j + 1][2]) * -p->theta_w + (p->fly_flag ? 0 :
((k[j + 2][0] * lsqr + k[j + 2][1] * l + k[j + 2][2]) * (chassis->target_dist - chassis->dist) +
(k[j + 3][0] * lsqr + k[j + 3][1] * l + k[j + 3][2]) * (chassis->target_v - chassis->vel) +
(k[j + 4][0] * lsqr + k[j + 4][1] * l + k[j + 4][2]) * -chassis->pitch +
(k[j + 5][0] * lsqr + k[j + 5][1] * l + k[j + 5][2]) * -chassis->pitch_w));
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p->T_wheel = T[0];
p->T_hip = T[1];
}