|
| 1 | +""" |
| 2 | +Pure business logic functions for flight controller operations. |
| 3 | +
|
| 4 | +This module contains stateless, side-effect-free functions that implement business rules |
| 5 | +and calculations. These functions are easily testable without needing hardware or mocks. |
| 6 | +
|
| 7 | +This file is part of ArduPilot Methodic Configurator. https://github.com/ArduPilot/MethodicConfigurator |
| 8 | +
|
| 9 | +SPDX-FileCopyrightText: 2024-2025 Amilcar do Carmo Lucas <amilcar.lucas@iav.de> |
| 10 | +
|
| 11 | +SPDX-License-Identifier: GPL-3.0-or-later |
| 12 | +""" |
| 13 | + |
| 14 | +from typing import Optional |
| 15 | + |
| 16 | + |
| 17 | +def calculate_voltage_thresholds(fc_parameters: dict[str, float]) -> tuple[float, float]: |
| 18 | + """ |
| 19 | + Calculate battery voltage thresholds for motor testing safety. |
| 20 | +
|
| 21 | + This is a pure function that extracts the minimum and maximum voltage thresholds |
| 22 | + from flight controller parameters. |
| 23 | +
|
| 24 | + Args: |
| 25 | + fc_parameters: Dictionary of flight controller parameters |
| 26 | +
|
| 27 | + Returns: |
| 28 | + tuple[float, float]: (min_voltage, max_voltage) for safe motor testing |
| 29 | +
|
| 30 | + Examples: |
| 31 | + >>> params = {"BATT_ARM_VOLT": 10.5, "MOT_BAT_VOLT_MAX": 25.2} |
| 32 | + >>> calculate_voltage_thresholds(params) |
| 33 | + (10.5, 25.2) |
| 34 | +
|
| 35 | + >>> calculate_voltage_thresholds({}) |
| 36 | + (0.0, 0.0) |
| 37 | +
|
| 38 | + """ |
| 39 | + min_voltage = fc_parameters.get("BATT_ARM_VOLT", 0.0) |
| 40 | + max_voltage = fc_parameters.get("MOT_BAT_VOLT_MAX", 0.0) |
| 41 | + return (min_voltage, max_voltage) |
| 42 | + |
| 43 | + |
| 44 | +def is_battery_monitoring_enabled(fc_parameters: dict[str, float]) -> bool: |
| 45 | + """ |
| 46 | + Check if battery monitoring is enabled in flight controller parameters. |
| 47 | +
|
| 48 | + Args: |
| 49 | + fc_parameters: Dictionary of flight controller parameters |
| 50 | +
|
| 51 | + Returns: |
| 52 | + bool: True if BATT_MONITOR != 0, False otherwise |
| 53 | +
|
| 54 | + Examples: |
| 55 | + >>> is_battery_monitoring_enabled({"BATT_MONITOR": 4.0}) |
| 56 | + True |
| 57 | +
|
| 58 | + >>> is_battery_monitoring_enabled({"BATT_MONITOR": 0.0}) |
| 59 | + False |
| 60 | +
|
| 61 | + >>> is_battery_monitoring_enabled({}) |
| 62 | + False |
| 63 | +
|
| 64 | + """ |
| 65 | + return fc_parameters.get("BATT_MONITOR", 0) != 0 |
| 66 | + |
| 67 | + |
| 68 | +def get_frame_info(fc_parameters: dict[str, float]) -> tuple[int, int]: |
| 69 | + """ |
| 70 | + Extract frame class and frame type from flight controller parameters. |
| 71 | +
|
| 72 | + Args: |
| 73 | + fc_parameters: Dictionary of flight controller parameters |
| 74 | +
|
| 75 | + Returns: |
| 76 | + tuple[int, int]: (frame_class, frame_type) |
| 77 | + frame_class: Frame class (default: 1 = QUAD) |
| 78 | + frame_type: Frame type (default: 1 = X) |
| 79 | +
|
| 80 | + Examples: |
| 81 | + >>> get_frame_info({"FRAME_CLASS": 1.0, "FRAME_TYPE": 3.0}) |
| 82 | + (1, 3) |
| 83 | +
|
| 84 | + >>> get_frame_info({}) |
| 85 | + (1, 1) |
| 86 | +
|
| 87 | + """ |
| 88 | + frame_class = int(fc_parameters.get("FRAME_CLASS", 1)) # Default to QUAD |
| 89 | + frame_type = int(fc_parameters.get("FRAME_TYPE", 1)) # Default to X |
| 90 | + return (frame_class, frame_type) |
| 91 | + |
| 92 | + |
| 93 | +def validate_battery_voltage( |
| 94 | + voltage: float, |
| 95 | + min_voltage: float, |
| 96 | + max_voltage: float, |
| 97 | +) -> tuple[bool, Optional[str]]: |
| 98 | + """ |
| 99 | + Validate if battery voltage is within safe operating range for motor testing. |
| 100 | +
|
| 101 | + Args: |
| 102 | + voltage: Current battery voltage in volts |
| 103 | + min_voltage: Minimum safe voltage (BATT_ARM_VOLT) |
| 104 | + max_voltage: Maximum safe voltage (MOT_BAT_VOLT_MAX) |
| 105 | +
|
| 106 | + Returns: |
| 107 | + tuple[bool, Optional[str]]: (is_valid, error_message) |
| 108 | + is_valid: True if voltage is within safe range |
| 109 | + error_message: None if valid, descriptive error message if invalid |
| 110 | +
|
| 111 | + Examples: |
| 112 | + >>> validate_battery_voltage(12.6, 10.5, 25.2) |
| 113 | + (True, None) |
| 114 | +
|
| 115 | + >>> validate_battery_voltage(9.0, 10.5, 25.2) |
| 116 | + (False, 'Battery voltage 9.00V is below minimum safe voltage 10.50V') |
| 117 | +
|
| 118 | + >>> validate_battery_voltage(26.0, 10.5, 25.2) |
| 119 | + (False, 'Battery voltage 26.00V is above maximum safe voltage 25.20V') |
| 120 | +
|
| 121 | + """ |
| 122 | + if voltage < min_voltage: |
| 123 | + return False, f"Battery voltage {voltage:.2f}V is below minimum safe voltage {min_voltage:.2f}V" |
| 124 | + if voltage > max_voltage: |
| 125 | + return False, f"Battery voltage {voltage:.2f}V is above maximum safe voltage {max_voltage:.2f}V" |
| 126 | + return True, None |
| 127 | + |
| 128 | + |
| 129 | +def convert_battery_telemetry_units( |
| 130 | + voltage_millivolts: int, |
| 131 | + current_centiamps: int, |
| 132 | +) -> tuple[float, float]: |
| 133 | + """ |
| 134 | + Convert battery telemetry from MAVLink units to standard units. |
| 135 | +
|
| 136 | + Args: |
| 137 | + voltage_millivolts: Battery voltage in millivolts (MAVLink BATTERY_STATUS.voltages) |
| 138 | + current_centiamps: Battery current in centiamps (MAVLink BATTERY_STATUS.current_battery) |
| 139 | +
|
| 140 | + Returns: |
| 141 | + tuple[float, float]: (voltage_volts, current_amps) |
| 142 | + voltage_volts: Voltage in volts |
| 143 | + current_amps: Current in amperes |
| 144 | +
|
| 145 | + Examples: |
| 146 | + >>> convert_battery_telemetry_units(12600, 1050) |
| 147 | + (12.6, 10.5) |
| 148 | +
|
| 149 | + >>> convert_battery_telemetry_units(-1, -1) # Invalid/unavailable readings |
| 150 | + (0.0, 0.0) |
| 151 | +
|
| 152 | + """ |
| 153 | + voltage = voltage_millivolts / 1000.0 if voltage_millivolts != -1 else 0.0 |
| 154 | + current = current_centiamps / 100.0 if current_centiamps != -1 else 0.0 |
| 155 | + return (voltage, current) |
| 156 | + |
| 157 | + |
| 158 | +def validate_throttle_percentage(throttle_percent: int) -> tuple[bool, Optional[str]]: |
| 159 | + """ |
| 160 | + Validate throttle percentage is within safe range for motor testing. |
| 161 | +
|
| 162 | + Args: |
| 163 | + throttle_percent: Throttle percentage (0-100) |
| 164 | +
|
| 165 | + Returns: |
| 166 | + tuple[bool, Optional[str]]: (is_valid, error_message) |
| 167 | + is_valid: True if throttle is valid |
| 168 | + error_message: None if valid, descriptive error message if invalid |
| 169 | +
|
| 170 | + Examples: |
| 171 | + >>> validate_throttle_percentage(50) |
| 172 | + (True, None) |
| 173 | +
|
| 174 | + >>> validate_throttle_percentage(0) |
| 175 | + (True, None) |
| 176 | +
|
| 177 | + >>> validate_throttle_percentage(-10) |
| 178 | + (False, 'Throttle percentage -10 is below minimum (0)') |
| 179 | +
|
| 180 | + >>> validate_throttle_percentage(150) |
| 181 | + (False, 'Throttle percentage 150 is above maximum (100)') |
| 182 | +
|
| 183 | + """ |
| 184 | + if throttle_percent < 0: |
| 185 | + return False, f"Throttle percentage {throttle_percent} is below minimum (0)" |
| 186 | + if throttle_percent > 100: |
| 187 | + return False, f"Throttle percentage {throttle_percent} is above maximum (100)" |
| 188 | + return True, None |
| 189 | + |
| 190 | + |
| 191 | +def validate_motor_test_duration(timeout_seconds: int) -> tuple[bool, Optional[str]]: |
| 192 | + """ |
| 193 | + Validate motor test duration is within safe limits. |
| 194 | +
|
| 195 | + Args: |
| 196 | + timeout_seconds: Test duration in seconds |
| 197 | +
|
| 198 | + Returns: |
| 199 | + tuple[bool, Optional[str]]: (is_valid, error_message) |
| 200 | + is_valid: True if duration is valid |
| 201 | + error_message: None if valid, descriptive error message if invalid |
| 202 | +
|
| 203 | + Examples: |
| 204 | + >>> validate_motor_test_duration(5) |
| 205 | + (True, None) |
| 206 | +
|
| 207 | + >>> validate_motor_test_duration(0) |
| 208 | + (False, 'Motor test duration 0 seconds is too short (minimum: 1 second)') |
| 209 | +
|
| 210 | + >>> validate_motor_test_duration(35) |
| 211 | + (False, 'Motor test duration 35 seconds is too long (maximum: 30 seconds)') |
| 212 | +
|
| 213 | + """ |
| 214 | + MIN_DURATION = 1 # noqa: N806 |
| 215 | + MAX_DURATION = 30 # noqa: N806 |
| 216 | + |
| 217 | + if timeout_seconds < MIN_DURATION: |
| 218 | + return False, f"Motor test duration {timeout_seconds} seconds is too short (minimum: {MIN_DURATION} second)" |
| 219 | + if timeout_seconds > MAX_DURATION: |
| 220 | + return False, f"Motor test duration {timeout_seconds} seconds is too long (maximum: {MAX_DURATION} seconds)" |
| 221 | + return True, None |
| 222 | + |
| 223 | + |
| 224 | +def calculate_motor_sequence_number(motor_index: int, zero_based: bool = True) -> int: |
| 225 | + """ |
| 226 | + Calculate MAVLink motor sequence number from motor index. |
| 227 | +
|
| 228 | + ArduPilot motor test command uses 1-based sequence numbers, |
| 229 | + but motor indices are often 0-based in user interfaces. |
| 230 | +
|
| 231 | + Args: |
| 232 | + motor_index: Motor index (0-based or 1-based depending on zero_based parameter) |
| 233 | + zero_based: If True, motor_index is 0-based; if False, motor_index is already 1-based |
| 234 | +
|
| 235 | + Returns: |
| 236 | + int: MAVLink motor sequence number (1-based) |
| 237 | +
|
| 238 | + Examples: |
| 239 | + >>> calculate_motor_sequence_number(0, zero_based=True) |
| 240 | + 1 |
| 241 | +
|
| 242 | + >>> calculate_motor_sequence_number(3, zero_based=True) |
| 243 | + 4 |
| 244 | +
|
| 245 | + >>> calculate_motor_sequence_number(1, zero_based=False) |
| 246 | + 1 |
| 247 | +
|
| 248 | + """ |
| 249 | + return motor_index + 1 if zero_based else motor_index |
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