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/*****************************************************************************
* Copyright Statement:
* --------------------
* This software is protected by Copyright and the information contained
* herein is confidential. The software may not be copied and the information
* contained herein may not be used or disclosed except with the written
* permission of MediaTek Inc. (C) 2005
*
* BY OPENING THIS FILE, BUYER HEREBY UNEQUIVOCALLY ACKNOWLEDGES AND AGREES
* THAT THE SOFTWARE/FIRMWARE AND ITS DOCUMENTATIONS ("MEDIATEK SOFTWARE")
* RECEIVED FROM MEDIATEK AND/OR ITS REPRESENTATIVES ARE PROVIDED TO BUYER ON
* AN "AS-IS" BASIS ONLY. MEDIATEK EXPRESSLY DISCLAIMS ANY AND ALL WARRANTIES,
* EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE IMPLIED WARRANTIES OF
* MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE OR NONINFRINGEMENT.
* NEITHER DOES MEDIATEK PROVIDE ANY WARRANTY WHATSOEVER WITH RESPECT TO THE
* SOFTWARE OF ANY THIRD PARTY WHICH MAY BE USED BY, INCORPORATED IN, OR
* SUPPLIED WITH THE MEDIATEK SOFTWARE, AND BUYER AGREES TO LOOK ONLY TO SUCH
* THIRD PARTY FOR ANY WARRANTY CLAIM RELATING THERETO. MEDIATEK SHALL ALSO
* NOT BE RESPONSIBLE FOR ANY MEDIATEK SOFTWARE RELEASES MADE TO BUYER'S
* SPECIFICATION OR TO CONFORM TO A PARTICULAR STANDARD OR OPEN FORUM.
*
* BUYER'S SOLE AND EXCLUSIVE REMEDY AND MEDIATEK'S ENTIRE AND CUMULATIVE
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*
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*
*****************************************************************************/
/*******************************************************************************
* Filename:
* ---------
* gps2lcsp_struct.h
*
* Project:
* --------
* MAUI
*
* Description:
* ------------
* This file is intends for local parameter declaration about GIS sap
*
* Author:
* -------
* -------
*
*==============================================================================
* HISTORY
* Below this line, this part is controlled by PVCS VM. DO NOT MODIFY!!
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*==============================================================================
*******************************************************************************/
#ifndef __GPS2LCSP_STRUCT_H__
#define __GPS2LCSP_STRUCT_H__
#include "gps2lcsp_enum.h"
#include "kal_public_api.h"
#include "kal_general_types.h"
#define GPS_ASSIST_DATA_SUB_ITEMS_FEILDS 16
#define GPS_ASSIST_DATA_N_SATE 8
#define GPS_ASSIST_DATA_N_SATE_DGPS 16
#define GPS_ASSIST_DATA_N_SATE_NAVIGATION_MODEL 16
#define GPS_ASSIST_DATA_N_SATE_ALMANAC 32 /* According to Stanley Huang: max almanac sat number = 32, not 64 */
#define GPS_ASSIST_DATA_N_SATE_ACQUISITION 16
#define GPS_ASSIST_DATA_N_SATE_RTI 16
#define GPS_ASSIST_DATA_N_SATE_MEAS 16 /* max allowed = 16, but typical = 4 to 12 */
#define GPS_ASSIST_DATA_N_SATE_TOW_ASSIST 16
#define GPS_ASSIST_CMD_TIMER_EXP_INTERVAL 1500
#define GPS_QUERY_TIMER_INTERVAL 500
#ifdef __AGPS_SUPPORT__
typedef struct
{
kal_uint8 semi_maj_uncertain; /* K1 = 0-127, mandotary, horizontal accuracy, need converted by 23.032 sec 6.2 */
kal_uint8 semi_min_uncertain; /* K2 = 0-127, mandotary, horizontal accuracy, need converted by 23.032 sec 6.2 */
kal_bool altitude_uncertain_valid; /* indicate if altitude_uncertain is valid */
kal_uint8 altitude_uncertain; /* K3 = 0-127, optional, vertical accuracy, need converted by 23.032 sec 6.4 */
kal_bool delay_valid; /* indiate if dealy is valid */
kal_uint32 delay; /* optional, response time ms*/
kal_bool age_valid; /* indicate if age field is valid, */
kal_uint16 age; /* 0 to 65535, optional, max location age, in sec */
kal_bool is_check_assist_data; /*set to TRUE will response error if assist data not enough */
kal_bool is_gsm_gps_ref_time_wanted; /* set to TRUE if GSM GPS ref time was required to be reported */
kal_bool is_utran_gps_ref_time_wanted; /*Set to TRUE if UTRAN GPS ref time was required to be reported */
/* uarfcn and phyCellId are valid when is_utran_gps_ref_time_wanted == KAL_TRUE */
kal_uint16 uarfcn;
kal_uint16 phyCellId;
} gps_pos_qop_struct;
typedef struct
{
kal_bool accuracy_valid;
kal_uint8 accuracy;
kal_uint32 delay; /* optional, response time ms*/
kal_bool is_check_assist_data; /*Set to TRUE will response error if assist data not enough */
kal_bool is_gsm_gps_ref_time_wanted; /* set to TRUE if GSM GPS ref time was required to be reported */
kal_bool is_utran_gps_ref_time_wanted; /*Set to TRUE if UTRAN GPS ref time was required to be reported */
/* uarfcn and phyCellId are valid when is_utran_gps_ref_time_wanted == KAL_TRUE */
kal_uint16 uarfcn;
kal_uint16 phyCellId;
} gps_meas_qop_struct;
typedef struct
{
kal_uint16 hor_speed; /*0-65536 .4remove and .5 add 1 unit is 1 km*/
} gps_h_velocity_struct;
typedef struct
{
kal_uint32 hor_speed; /*unit is 0.1 km*/
kal_uint32 ver_speed; /*unit is 0.1 km*/
} gps_hv_velocity_struct;
typedef struct
{
kal_uint32 hor_speed; /*unit is 0.1 km*/
kal_uint32 hor_speed_uncertainty;
} gps_h_velocity_uncert_struct;
typedef struct
{
kal_uint32 ver_direction; /*degree*/
kal_uint32 hor_speed; /*unit is 0.1 km*/
kal_uint32 ver_speed; /*unit is 0.1 km*/
kal_uint32 hor_speed_uncertainty;
kal_uint32 ver_speed_uncertainty;
} gps_hv_velocity_uncert_struct;
typedef struct
{
gps_velocity_type_enum type;
union
{
gps_h_velocity_struct hor_velocity;
gps_hv_velocity_struct hv_velocity;
gps_h_velocity_uncert_struct hor_uncertainty;
gps_hv_velocity_uncert_struct hv_uncertainty;
} v;
} gps_velocity_struct;
typedef struct
{
kal_uint8 type; /* only "ellipsoid point with altitude and uncertainty ellipsoid"
type (1001b) is supported*/
kal_bool sign_latitude; /* true: SOUTH, false: NORTH */
kal_uint32 latitude; /* N1, encoded latitude */
kal_uint32 longtitude; /* N2, encoded longtitude with 2's complement */
kal_bool sign_altitude; /* true: DEPTH, false: HEIGHT */
kal_uint16 altitude; /* no encoding, unit in meter */
kal_uint8 unc_major; /* K1, encoded r1 */
kal_uint8 unc_minor; /* K2, encoded r2 */
kal_uint8 unc_bear; /* N3, encoded a = 2N3, Bearing of semi-major axis (degrees)*/
kal_uint8 unc_altitude; /* K3, encode r3, vertical uncertain */
kal_uint8 confidence; /* %, The confidence by which the position of a target
entity is known to be within the shape description,
expressed as a percentage. [0 ~ 100] (%)*/
gps_velocity_struct velocity; /*only support horizontal speed*/
kal_uint16 bearing; /*0-360 Direction of the horizontal speed*/
} gps_gad_pos_estimate_struct;
/* in position or measurement result */
typedef struct
{
kal_uint16 ref_time_ms_part;
kal_uint32 ref_time_ls_part;
kal_uint16 uarfcn;
kal_uint16 phyCellId; // Must valid value
kal_uint16 sfn;
kal_bool ref_time_uncertain_valid;
kal_uint8 ref_time_uncertain;
} utran_gps_ref_time_result_struct;
typedef struct
{
kal_uint16 ref_frame; /* If refFrame is within (42432..65535), it shall be ignored by the receiver */
kal_uint16 week; /*gps week*/
kal_uint32 tow; /*msec*/
/* GPS TOW [0 ~ 14399999] (msec) for which the location
estimate is valid, rounded down to the nearest
millisecond unit. RRLP Location Information element
only contains the 24 LSBs of GPS TOW. */
kal_uint8 fix_type; /* position fix type performed by the GPS receiver:
'0' = 2D fix '1' = 3D fix*/
gps_gad_pos_estimate_struct pos_estimate;
} gps_pos_result_struct;
typedef struct
{
kal_uint8 sat_id; /*The particular satellite for which the measurement data is valid. [1 ~ 32]*/
kal_uint8 carrier_noise; /*The estimate of the carrier-to-noise ratio of the received signal from the particular satellite used in the measurement. [0 ~ 63] (dB-Hz)*/
kal_uint16 doppler; /*0.2 Hz The Doppler measured by the MS for the particular satellite signal. [-32768 ~ 32767]*/
kal_uint16 whole_chips; /*chips The whole value of the code-phase measurement made by the GPS receiver for the particular satellite signal at the time of measurement. [0 ~ 1022] (chips)*/
kal_uint16 fractional_chips; /*2^-10 chips The fractional value of the code-phase measurement made by the GPS receiver for the particular satellite signal at the time of measurement. (2^-10 C/A chips) [0 ~ 1023]*/
kal_uint8 multipath; /*The multipath Indicator value. Possible values are listed below:
'0' = Not measured
'1' = Low, MP error < 5m
'2' = Medium, 5m < MP error < 43m
'3' = High, MP error > 43m*/
kal_uint8 pseudorang_m; /*Pseudorange RMS Error Mantissa*/
kal_uint8 pseudorang_e; /*Pseudorange RMS Error Exponent*/
} gps_meas_para_struct;
typedef struct
{
kal_uint16 ref_frame; /* If refFrame is within (42432..65535), it shall be ignored by the receiver */
kal_uint32 tow;
/*GPS TOW [0 ~ 14399999] (msec) for which the location estimate is valid, rounded down to the nearest millisecond unit.
RRLP GPS Measurement Information element only contains the 24 LSBs of GPS TOW.*/
kal_uint8 sate_num;/*The number of GPS measurements for which measurement satellites are provided at the time of measurement*/
gps_meas_para_struct meas_param[GPS_ASSIST_DATA_N_SATE_MEAS];
} gps_meas_result_struct;
typedef struct
{
kal_uint8 sv; /* sat id, 6 bits */
kal_uint32 wn; /* 10 bits, set to 0 */
kal_uint8 c_a; /*2 bits*/
kal_uint8 ura; /*4 bits*/
kal_uint8 sv_health; /*6 bits*/
kal_uint16 iodc; /*10 bits*/
kal_uint8 l2p; /* 1 bits */
kal_uint32 sf1_23msb; /* 23/87 bits, MSB */
kal_uint32 sf1_24mb1; /* 24/87 bits */
kal_uint32 sf1_24mb2; /* 24/87 bits */
kal_uint16 sf1_16lsb; /* 16/87 bits, LSB */
kal_int8 tgd; /* 8 bits */
kal_uint16 toc; /*16 bits*/
kal_int8 af2; /* 8 bits */
kal_int16 af1; /* 16 bits */
kal_int32 af0; /* 22 bits */
kal_uint8 iode; /* 8 bits, set to iodc 8bit lsb */
kal_int16 crs; /* 16 bits */
kal_int16 delta_n; /* 16 bits */
kal_int32 m0; /* 32 bits */
kal_int16 cuc; /* 16 bits */
kal_uint32 e; /*32 bits*/
kal_int16 cus; /* 16 bits */
kal_uint32 sqrt_a; /*32 bits*/
kal_uint16 toe; /*16 bits*/
kal_uint8 fit; /* 1 bits */
kal_uint8 aodo; /*5 bits*/
kal_int16 cic; /* 16 bits */
kal_int32 omega0; /* 32 bits */
kal_int16 cis; /* 16 bits */
kal_int32 i0; /* 32 bits */
kal_int16 crc; /* 16 bits */
kal_int32 w; /* 32 bits */
kal_int32 omega_dot; /* 24 bits */
kal_int16 idot; /* 14 bits */
} gps_assist_navigation_model_single_struct;
/*ephemeris in GPS chip AGPS_P710*/
typedef struct
{
kal_uint8 n_sat;
gps_assist_navigation_model_single_struct
navigation_data[GPS_ASSIST_DATA_N_SATE_NAVIGATION_MODEL];
} gps_assist_navigation_model_struct;
/*ephemeris in GPS chip AGPS_P710*/
typedef struct
{
kal_uint8 data_id; /*2 bits set to 01*/
kal_uint8 sat_id; /*6 bits*/
kal_uint16 e; /*16 bits*/
kal_uint8 toa; /*8 bits*/
kal_int16 delta_i; /*16 bits*/
kal_int16 omega_dot; /*16 bits*/
kal_uint8 sv_health; /*8 bits*/
kal_uint32 sqrt_a; /*24 bits*/
kal_int32 omega0; /*24 bits*/
kal_int32 w; /*24 bits*/
kal_int32 m0; /*24 bits*/
kal_int16 af0; /*11 bits*/
kal_int16 af1; /*11 bits*/
} gps_assist_almanac_single_struct;
typedef struct
{
kal_uint8 n_sat;
kal_uint8 week; /*Almanac reference GPS week number*/
gps_assist_almanac_single_struct almanac_data[GPS_ASSIST_DATA_N_SATE_ALMANAC];
} gps_assist_almanac_struct;
typedef struct
{
kal_uint16 tlm_word; /*telemetry message[0-16383]*/
kal_uint8 sat_id; /*Sate PRN [1-32]*/
kal_uint8 anti_spoof; /*anti spoof flag[0,1]*/
kal_uint8 alert; /*alert flag*/
kal_uint8 tlm_rsvd_bits; /*2 bit reserved bits[0-3]*/
} gps_assist_tow_assist_struct;
//In "ref time" or "aquisition assitance"
typedef struct
{
kal_uint16 ref_time_ms_part;
kal_uint32 ref_time_ls_part;
kal_uint16 uarfcn;
kal_uint16 phyCellId; // Must valid value
kal_uint16 sfn;
uagps_cp_sfn_tow_uncertainty_type sfn_tow_uncentainty_type;
/* if type is UAGPS_CP_SFN_TOW_UNCERTAINTY_10MS_THRESHOLD, 0 for UAGPS_CP_SFN_TOW_UNCERTAINTY_LESS_THAN_10, 1 for UAGPS_CP_SFN_TOW_UNCERTAINTY_MORE_THAN_10,
if type is UAGPS_CP_SFN_TOW_UNCERTAINTY_MICROSECOND, unit is microsecond,
else don't care this field */
kal_uint32 sfn_tow_Uncertainty;
kal_bool utran_gps_driftrate_valid;
uagps_cp_utran_gps_driftrate utran_gps_driftrate;
} utran_gps_ref_time_struct;
typedef struct
{
kal_uint16 bcch_carrier; /* BCCH Carrier of 2G serving cell: 0~1023 */
kal_uint8 bsic; /* BSIC of 2G serving cell: 0~63 */
kal_uint32 FNm; /* FNm (frame number with MSB is truncated): 0~(2^21-1) */
kal_uint8 tn; /* TN (timeslot number): 0~7 */
kal_uint8 bn; /* BN (bit number): 0~156 */
} gsm_gps_ref_time_struct;
typedef struct
{
kal_uint16 week; /*GPS week number spec not said range*/
kal_uint32 tow; /*unit0.08 GPS time of week of the transmission of the $ character at the start of the message [0 ~ 604800]*/
kal_uint16 tow_rms; /*set to 3000*/
kal_uint16 fs_tow; /*set to 0*/
kal_uint16 fs_rms; /*set to 0*/
kal_uint8 n_sat; /*number of tow assist sates*/
gps_assist_tow_assist_struct tow_assist[GPS_ASSIST_DATA_N_SATE_TOW_ASSIST];
/* 2G Timing Sync. Info */
kal_bool gsm_gps_ref_time_valid;
gsm_gps_ref_time_struct gsm_gps_ref_time;
/* 3G Timing Sync. Info */
kal_bool utran_gps_ref_time_valid;
utran_gps_ref_time_struct utran_gps_ref_time;
} gps_assist_ref_time_struct;
typedef struct
{
kal_bool sign_latitude; /* true: SOUTH, false: NORTH */
kal_uint32 latitude; /* N1, encoded latitude */
kal_uint32 longitude; /* N2, encoded longtitude with 2's complement */
kal_bool sign_altitude; /* true: DEPTH, false: HEIGHT */
kal_uint16 altitude; /* no encoding, unit in meter */
kal_uint16 unc_smaj; /* in m */
kal_uint16 unc_smin; /* in m */
kal_uint16 bearing; /* in degree */
kal_uint16 unc_vert; /* in m, uncertain altitue */
kal_uint8 confidence; /* 0 to 100, in % */
} gps_assist_ref_location_struct;
typedef struct
{
kal_int8 a0; /*Alpha0 (x 2^-30 seconds)*/
kal_int8 a1; /*Alpha1 (x 2^-27 seconds per semicircle)*/
kal_int8 a2; /*Alpha2 (x 2^-24 seconds per semicircle ^2)*/
kal_int8 a3; /*Alpha3 (x 2^-24 seconds per semicircle ^3)*/
kal_int8 b0; /*Beta0 (x 2 ^ 11 seconds)*/
kal_int8 b1; /*Beta1 (x 2 ^ 14 seconds per semicircle)*/
kal_int8 b2; /*Beta2 (x 2 ^ 16 seconds per semicircle ^2)*/
kal_int8 b3; /*Beta3 (x 2 ^ 16 seconds per semicircle ^3)*/
} gps_assist_ionosphere_struct;
typedef struct
{
kal_int32 a1;
kal_int32 a0;
kal_uint8 tot;
kal_uint8 wnt;
kal_int8 delta_ls;
kal_uint8 wnlsf;
kal_int8 dn;
kal_int8 delta_lsf;
} gps_assist_utc_struct;
typedef struct
{
kal_uint8 number_bad;
kal_uint8 bad_svid[GPS_ASSIST_DATA_N_SATE_RTI]; /* 6 bits for each sat */
} gps_assist_real_time_integrity_struct;
typedef struct
{
kal_uint8 sv_id; /*Satellite PRN number [1~32]*/
kal_int16 dopp0; /*unit 2.5Hz, 0th order term of satellite Doppler [-2048 ~ 2047]*/
kal_int8 dopp1; /*unit 1/42Hz, 1th order term of satellite Doppler [-42.0 ~ 21]*/
kal_uint8 dopp_sr; /*Doppler search range [2^-n * (200) Hz, n = 0 - 4]*/
kal_uint16 code_p; /*GPS satellite code chips [0 ~ 1022] (chip)*/
kal_uint8 int_code; /*Integer code phase [0 ~ 19]*/
kal_uint8 bit; /*GPS bit number [0 ~ 3]*/
kal_uint8 code_sr; /*Code phase search window [GPS task will lookup table covert to 1 ~ 512]*/
kal_uint8 azimuth; /*unit 11.25 deg,Satellite azimuth angle [0 ~ 31]*/
kal_uint8 elevation; /*unit 11.25 deg, Satellite elevation angle [0 ~ 7]*/
} gps_assist_acquisition_single_struct;
typedef struct
{
kal_uint8 n_sat; /* 4 bits */
kal_uint32 tow; /*unit 0.08sec, GPS time of week [0 ~ 7559999] 23bits*/
gps_assist_acquisition_single_struct sate_data[GPS_ASSIST_DATA_N_SATE_ACQUISITION];
/* 2G Timing Sync. Info */
kal_bool gsm_gps_ref_time_valid;
gsm_gps_ref_time_struct gsm_gps_ref_time;
/* 3G Timing Sync. Info */
kal_bool utran_gps_ref_time_valid;
utran_gps_ref_time_struct utran_gps_ref_time;
} gps_assist_acquisition_struct;
typedef struct
{
kal_uint8 sat_id; /*Satellite PRN for which the corrections are applicable [1 ~ 32]*/
kal_uint8 iode; /*The sequence number [0 ~ 255] for the sphemeris for the particular satellite.*/
kal_uint8 udre; /*Provides an estimate [0 ~ 3] of the uncertainty (1-sigma) in the corrections for the particular satellite.*/
kal_int16 prc; /*Unit 0.32m, The correction [+/-2047] to the pseudorange for the particular satellite at the GPS Reference Time.*/
kal_int8 rrc; /*Unit 0.032m, The rate of change of the pseudorange correction [+/- 127] for the particular satellite.*/
} gps_assist_dgps_sate_data_struct;
typedef struct
{
kal_uint32 tow; /*Unit sec, GPS TOW [0 ~ 604799] indicates the baseline time for which the corrections are valid*/
kal_uint8 status; /*This field indicates the status [0 ~ 7] of the differential corrections contained in the broadcast message. The "UDRE Factor" value is applied to the UDRE values contained in the message.*/
kal_uint8 n_sat; /*The number of satellites for which differential corrections are available. Corrections for up to 11 satellites.*/
gps_assist_dgps_sate_data_struct sat_data[GPS_ASSIST_DATA_N_SATE_DGPS];
} gps_assist_dgps_correction_struct;
typedef struct
{
kal_uint16 ref_bcch_carrier; /* ARFCN of current serving cell */
kal_uint8 ref_bsic; /* BSIC of current serving cell */
} gps_gsm_loc_info_struct;
typedef struct
{
kal_bool ref_frame_msb_valid;
kal_uint8 ref_frame_msb;
kal_bool tow_subms_valid;
kal_uint16 tow_subms;
kal_bool delta_tow_valid;
kal_uint8 delta_tow;
kal_bool ref_time_unc_valid;
kal_uint8 ref_time_unc;
} gsm_gps_ref_time_result_struct;
typedef struct
{
kal_uint16 w_n;
kal_uint16 toe;
kal_uint8 n_sat;
kal_uint8 limit;
kal_uint8 sat_id[GPS_ASSIST_DATA_SUB_ITEMS_FEILDS];
kal_uint16 iode[GPS_ASSIST_DATA_SUB_ITEMS_FEILDS];
} gps_sat_related_data_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
kal_bool req_time_assist_meas;
kal_bool environment_valid;
kal_uint8 environment;
gps_pos_qop_struct qop;
lcs_sim_source_enum sim_source; /* for Gemini SIM1/SIM2 */
/**
* Doug 20130326
* CP Auto Reset refine for OTA TIS 3G:
* if network does not sent RESET msg, periodicalReporting with reportingAmount is ra1
* autoResetTrigger is set to TRUE, and inform GPS task within POS(MEAS)_GAD_REQ.
*/
kal_bool autoResetTrigger;
} gps_pos_gad_req_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
gps_error_code_enum error_code;
kal_bool bitmap_valid;
kal_uint16 bitmap;
gps_sat_related_data_struct sat_data;
gps_pos_result_struct pos_result;
kal_bool gsm_loc_info_valid;
gps_gsm_loc_info_struct gsm_loc_info; /* for 2G ref. time timing sync. to indicate the serving cell */
kal_bool gsm_gps_ref_time_result_valid;
gsm_gps_ref_time_result_struct gsm_gps_ref_time_result;
kal_bool utran_gps_ref_time_result_valid;
utran_gps_ref_time_result_struct utran_gps_ref_time_result;
} gps_pos_gad_cnf_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
kal_bool req_time_assist_meas;
kal_bool environment_valid;
kal_uint8 environment;
gps_meas_qop_struct qop;
lcs_sim_source_enum sim_source; /* for Gemini SIM1/SIM2 */
/**
* Doug 20130326
* CP Auto Reset refine for OTA TIS 3G:
* if network does not sent RESET msg, periodicalReporting with reportingAmount is ra1
* autoResetTrigger is set to TRUE, and inform GPS task within POS(MEAS)_GAD_REQ.
*/
kal_bool autoResetTrigger;
} gps_lcsp_meas_gad_req_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
gps_error_code_enum error_code;
kal_bool bitmap_valid;
kal_uint16 bitmap;
gps_sat_related_data_struct sat_data;
gps_meas_result_struct meas_result;
kal_bool gsm_loc_info_valid;
gps_gsm_loc_info_struct gsm_loc_info; /* for 2G ref. time timing sync. to indicate the serving cell */
kal_bool gsm_gps_ref_time_result_valid;
gsm_gps_ref_time_result_struct gsm_gps_ref_time_result;
kal_bool utran_gps_ref_time_result_valid;
utran_gps_ref_time_result_struct utran_gps_ref_time_result;
} gps_lcsp_meas_gad_cnf_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
} gps_lcsp_abort_req_struct;
typedef struct
{
LOCAL_PARA_HDR
} gps_lcsp_agps_restart_ind_struct;
typedef union {
gps_assist_navigation_model_struct navigation_model;
gps_assist_almanac_struct almanac;
gps_assist_ref_time_struct ref_time;
gps_assist_ref_location_struct ref_location;
gps_assist_ionosphere_struct ionosphere;
gps_assist_utc_struct utc;
gps_assist_dgps_correction_struct dgps;
gps_assist_acquisition_struct acquisition;
gps_assist_real_time_integrity_struct rti;
} assist_data_union;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
kal_bool req_time_assist_meas;
gps_assist_data_type_enum type;
assist_data_union assist_data;
kal_bool ref_time_uncertain_valid;
kal_uint32 ref_time_uncertain;
lcs_sim_source_enum sim_source; /* for Gemini SIM1/SIM2 */
} gps_lcsp_assist_data_req_struct;
typedef struct
{
LOCAL_PARA_HDR
kal_uint8 transaction_id;
gps_assist_data_type_enum type;
gps_result_enum result;
} gps_lcsp_assist_data_cnf_struct;
#endif /*__AGPS_SUPPORT__*/
#endif /*__GPS2LCSP_STRUCT_H__*/