Paparazzi UAS
v5.18.0_stable
Paparazzi is a free software Unmanned Aircraft System.
vi_datalink.h
Go to the documentation of this file.
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/*
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* Copyright (C) 2010 The Paparazzi Team
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*
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* This is the implementation of the "external interface" to the autopilot.
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* using datalink messages.
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*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 2 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program; if not, write to the Free Software
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* Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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#ifndef VEHICLE_INTERFACE_DATALINK_H
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#define VEHICLE_INTERFACE_DATALINK_H
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#include "
std.h
"
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#include "
modules/vehicle_interface/vi.h
"
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#include "
math/pprz_algebra_int.h
"
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#ifndef VI_MAX_H_SPEED
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#define VI_MAX_H_SPEED 4.
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#endif
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#ifndef VI_MAX_V_SPEED
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#define VI_MAX_V_SPEED 2.
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#endif
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#ifndef VI_MAX_HEADING_RATE
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#define VI_MAX_HEADING_RATE RadOfDeg(60.)
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#endif
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extern
void
vi_update_wp
(
uint8_t
wp_id);
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#ifdef VI_PHI_THETA_MAX
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#define VI_LIMIT_ATTITUDE(_att) { \
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BoundAbs(_att.phi, VI_PHI_THETA_MAX); \
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BoundAbs(_att.theta, VI_PHI_THETA_MAX); \
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}
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#else
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#define VI_LIMIT_ATTITUDE(_x) {}
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#endif
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#define VI_PARSE_DATALINK(_dl_buffer) { \
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vi.last_msg = 0; \
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vi.input.h_mode = DL_BOOZ2_FMS_COMMAND_h_mode(_dl_buffer); \
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vi.input.v_mode = DL_BOOZ2_FMS_COMMAND_v_mode(_dl_buffer); \
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switch (vi.input.h_mode) { \
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case GUIDANCE_H_MODE_KILL: \
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case GUIDANCE_H_MODE_RATE : \
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break; \
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case GUIDANCE_H_MODE_ATTITUDE : \
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{ \
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vi.input.h_sp.attitude.phi = DL_BOOZ2_FMS_COMMAND_h_sp_1(_dl_buffer); \
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vi.input.h_sp.attitude.theta = DL_BOOZ2_FMS_COMMAND_h_sp_2(_dl_buffer); \
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vi.input.h_sp.attitude.psi = DL_BOOZ2_FMS_COMMAND_h_sp_3(_dl_buffer); \
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ANGLE_REF_NORMALIZE(vi.input.h_sp.attitude.psi); \
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VI_LIMIT_ATTITUDE(vi.input.h_sp.attitude); \
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} \
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break; \
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case GUIDANCE_H_MODE_HOVER : \
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{ \
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vi.input.h_sp.pos.x = DL_BOOZ2_FMS_COMMAND_h_sp_1(_dl_buffer); \
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vi.input.h_sp.pos.y = DL_BOOZ2_FMS_COMMAND_h_sp_2(_dl_buffer); \
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} \
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break; \
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case GUIDANCE_H_MODE_NAV : \
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{ \
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vi.input.h_sp.speed.x = DL_BOOZ2_FMS_COMMAND_h_sp_1(_dl_buffer); \
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vi.input.h_sp.speed.y = DL_BOOZ2_FMS_COMMAND_h_sp_2(_dl_buffer); \
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vi.input.h_sp.speed.z = DL_BOOZ2_FMS_COMMAND_h_sp_3(_dl_buffer); \
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} \
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break; \
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default: \
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break; \
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} \
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switch (vi.input.v_mode) { \
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case GUIDANCE_V_MODE_KILL: \
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case GUIDANCE_V_MODE_RC_DIRECT: \
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case GUIDANCE_V_MODE_RC_CLIMB: \
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break; \
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case GUIDANCE_V_MODE_CLIMB : \
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vi.input.v_sp.climb = DL_BOOZ2_FMS_COMMAND_v_sp(_dl_buffer); \
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break; \
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case GUIDANCE_V_MODE_HOVER : \
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vi.input.v_sp.height = DL_BOOZ2_FMS_COMMAND_v_sp(_dl_buffer); \
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break; \
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case GUIDANCE_V_MODE_NAV : \
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vi.input.v_sp.climb = DL_BOOZ2_FMS_COMMAND_v_sp(_dl_buffer); \
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break; \
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default: \
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break; \
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} \
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}
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#define VI_NAV_STICK_PARSE_DL(_dl_buffer) { \
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vi.last_msg = 0; \
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vi.input.h_mode = GUIDANCE_H_MODE_NAV; \
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vi.input.v_mode = GUIDANCE_V_MODE_NAV; \
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vi.input.h_sp.speed.x = DL_BOOZ_NAV_STICK_vx_sp(_dl_buffer); \
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vi.input.h_sp.speed.y = DL_BOOZ_NAV_STICK_vy_sp(_dl_buffer); \
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vi.input.h_sp.speed.z = DL_BOOZ_NAV_STICK_r_sp(_dl_buffer); \
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vi.input.v_sp.climb = DL_BOOZ_NAV_STICK_vz_sp(_dl_buffer); \
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}
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#define NavUpdateWPFromVI(_wp) { if (vi.enabled) { vi_update_wp(uint8_t _wp); } }
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#endif
/* VI_DATALINK_H */
vi_update_wp
void vi_update_wp(uint8_t wp_id)
Definition:
vi_datalink.c:42
pprz_algebra_int.h
Paparazzi fixed point algebra.
std.h
uint8_t
unsigned char uint8_t
Definition:
types.h:14
vi.h
sw
airborne
modules
vehicle_interface
vi_datalink.h
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