Adafruit_Learning_System_Gu.../Asteroid_Tracker/code.py
2025-04-07 15:14:31 -04:00

161 lines
5.9 KiB
Python

# SPDX-FileCopyrightText: 2025 Liz Clark for Adafruit Industries
#
# SPDX-License-Identifier: MIT
import os
import time
import ssl
import board
import wifi
import socketpool
import microcontroller
import displayio
from adafruit_display_text.bitmap_label import Label
from adafruit_bitmap_font import bitmap_font
import adafruit_imageload
from fourwire import FourWire
import adafruit_requests
from adafruit_gc9a01a import GC9A01A
from adafruit_ticks import ticks_ms, ticks_add, ticks_diff
cad_url = ("https://ssd-api.jpl.nasa.gov/cad.api?"
"des=2024%20YR4&body=ALL&"
"date-min=2030-01-01&date-max=2060-01-01")
sentry_url = "https://ssd-api.jpl.nasa.gov/sentry.api?des=2024%20YR4"
# connect to wifi
try:
wifi.radio.connect(os.getenv('CIRCUITPY_WIFI_SSID'), os.getenv('CIRCUITPY_WIFI_PASSWORD'))
except TypeError:
print("Could not find WiFi info. Check your settings.toml file!")
raise
context = ssl.create_default_context()
with open("/ssd-api-jpl-nasa-gov-chain.pem", "rb") as certfile:
context.load_verify_locations(cadata=certfile.read())
pool = socketpool.SocketPool(wifi.radio)
requests = adafruit_requests.Session(pool, context)
spi = board.SPI()
tft_cs = board.TX
tft_dc = board.RX
tft_reset = None
displayio.release_displays()
display_bus = FourWire(spi, command=tft_dc, chip_select=tft_cs, reset=tft_reset)
display = GC9A01A(display_bus, width=240, height=240, auto_refresh=False)
main_group = displayio.Group()
display.root_group = main_group
bitmap_bg, palette_bg = adafruit_imageload.load("/earth_bg.bmp",
bitmap=displayio.Bitmap,
palette=displayio.Palette)
grid_bg = displayio.TileGrid(bitmap_bg, pixel_shader=palette_bg)
main_group.append(grid_bg)
font = bitmap_font.load_font('/Arial-14.bdf')
name_area = Label(font, text="2024 YR4", color=0xFFFFFF, background_color=0x000000)
name_area.anchored_position = (display.width / 2, 0)
name_area.anchor_point = (0.5, 0.0)
date_area = Label(font, text="2032-12-22", color=0xFFFFFF, background_color=0x000000)
date_area.anchored_position = (display.width / 2, name_area.height+10)
date_area.anchor_point = (0.5, 0.0)
moon_area = Label(font, text="Moon: ", color=0xFFFFFF, background_color=0x000000)
moon_area.anchored_position = (display.width / 2, name_area.height+10 + date_area.height+5)
moon_area.anchor_point = (0.5, 0.0)
earth_area = Label(font, text="Earth: ", color=0xFFFFFF, background_color=0x000000)
earth_area.anchored_position = (display.width / 2, name_area.height+10 +
moon_area.height+5 +
date_area.height + 5)
earth_area.anchor_point = (0.5, 0.0)
impact_area = Label(font, text="Earth Impact: 0.0000%", color=0xFFFFFF, background_color=0x000000)
impact_area.anchored_position = (display.width / 2, name_area.height+10 +
moon_area.height+5 +
earth_area.height + 5 +
date_area.height + 5)
impact_area.anchor_point = (0.5, 0.0)
main_group.append(impact_area)
main_group.append(earth_area)
main_group.append(moon_area)
main_group.append(date_area)
main_group.append(name_area)
bit_asteroid, pal_asteroid = adafruit_imageload.load("/asteroid.bmp",
bitmap=displayio.Bitmap,
palette=displayio.Palette)
asteroid = displayio.TileGrid(bit_asteroid, pixel_shader=pal_asteroid,
x = 25, y=100)
pal_asteroid.make_transparent(0)
main_group.append(asteroid)
def diagonal_travel(bitmap_object, start_x=-59, start_y=-59, end_x=240, end_y=240, delay=0.01):
# Set initial position
bitmap_object.x = start_x
bitmap_object.y = start_y
# Calculate total movement distance
distance_x = end_x - start_x
distance_y = end_y - start_y
# Calculate number of steps (use the larger distance)
steps = max(abs(distance_x), abs(distance_y)) // 1
# Calculate step size for each axis to maintain diagonal movement
step_x = distance_x / steps
step_y = distance_y / steps
# Animate the movement
for i in range(steps + 1):
# Update position
bitmap_object.x = int(start_x + (step_x * i))
bitmap_object.y = int(start_y + (step_y * i))
display.refresh()
# Pause to control animation speed
time.sleep(delay)
def au_to_miles(au):
# 1 AU = 92,955,807 miles
miles_per_au = 92955807
return au * miles_per_au
timer_clock = ticks_ms()
timer = 3600 * 1000
first_run = True
while True:
try:
if first_run or ticks_diff(ticks_ms(), timer_clock) >= timer:
sentry_response = requests.get(sentry_url)
sentry_json = sentry_response.json()
impact = sentry_json['summary']['ip']
sentry_response.close()
overall_ip = float(impact) * 100
cad_response = requests.get(cad_url)
cad_json = cad_response.json()
earth_distance = au_to_miles(float(cad_json['data'][0][4]))
earth_area.text = f"{cad_json['data'][0][10]}: {int(earth_distance)} mi"
moon_distance = au_to_miles(float(cad_json['data'][1][4]))
moon_area.text = f"{cad_json['data'][1][10]}: {int(moon_distance)} mi"
date = cad_json['data'][0][3]
date = date.split()
date_area.text = f"{date[0]}"
cad_response.close()
impact_area.text = f"Earth Impact: {overall_ip:.4f}%"
display.refresh()
timer_clock = ticks_add(timer_clock, timer)
diagonal_travel(asteroid, start_x=-45, start_y=300, end_x=300, end_y=-45)
time.sleep(0.1)
# pylint: disable=broad-except
except Exception as e:
print("Error:\n", str(e))
print("Resetting microcontroller in 10 seconds")
time.sleep(10)
microcontroller.reset()