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authorDawsyn Schraiber <[email protected]>2024-05-09 02:05:35 -0400
committerGitHub <[email protected]>2024-05-09 02:05:35 -0400
commit93acde052369568beaefb0d99629d8797f5c191f (patch)
treea3fb96ddad2d289aa7f8bf410c60cf6289bca7a1 /include/unused/rocketUtils.hpp
parent5f68c7a1b5c8dec82d4a2e1e12443a41b5196b1d (diff)
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Raspberry Pi Pico (#12)
* Adding a 90% completed, compilable but untested ADS * Made basic changes to actuator & sensor. Also added motor class * Removed unnecessary .cpp files * Updated sensor & actuator classes, finished ads, added variable time step to kalman filter, set up all tests for future assertions * Relocated 'main' to 'active-drag-system.cpp'. Added more info to README * Removed main.cpp * Added more details to README * Changed some function parameters from pass-by-pointer to pass-by-reference. Also removed the std namespace * Started writing the test cases * Updated the .gitignore file * Removed some files that should be gitignored * Up to date with Jazz's pull request * Test Launch Branch Created; PRU Servo Control with Test Program * Added I2C device class and register IDs for MPL [INCOMPLETE SENSOR IMPLEMENTATION] Needs actual data getting function implementation for both sensors and register IDs for BNO, will implement shortly. * Partial implementation of MPL sensor Added startup method, still needs fleshed out data getters and setters and finished I2C implementation. MOST LIKELY WILL HAVE COMPILATION ISSUES. * *Hypothetically* complete MPL implementation NEEDS HARDWARE TESTING * IMU Header and init() method implementation Needs like, all data handling still lol * Hypothetically functional (Definitely won't compile) * We ball? * Conversion to Raspberry Pi Pico Build System; Removed Beaglebone specific code; Simple blinking example in ADS source file; builds for Pico W * Rearranged build so dependent upon cmake file already existing in pico-sdk; current executable prints current altitude, velocity, and time taken to read and calculate said values; ~320 us to do so * Altimeter interrupt callback for Pad to Boost State; dummy templates for other callbacks with comments describing potential implementation details * Altimeter interrupts relatively finished; need to test with vacuum chamber to verify behavior * Established interrupt pins as pullup and active-low; adjusted callback functions to properly use function pointers; still need to verify interrupt system with vacuum chamber * Removed weird artifact in .gitignore, adjust CMakeLists to auto pull pico sdk, added Dockerfile * added Docker dev container file * modified CMakeLists to auto pull sdk if not already downloaded, add build.sh script, fixed Dockerfile * added bno055 support * changed bno055 lin accel struct to use float instead of double * added bno055 support not tested, but compiles, fixed CMakLists to before I messed with it * added absolute quaternion output from bno055 * Added Euler and aboslute linear accelration * Flash implementation for data logging; each log entry is 32 bytes long * added base pwm functions and started on apogee detection * State machine verified functional with logging capabilities; currently on same core * Ooops missed double define, renamed LOOP_HZ to LOOP_PERIOD; State machine functional after merge still * Simple test program to see servo PWM range; logging with semaphores for safe multithreading * Kalman filters generously provided from various sources for temporary replacement; minimum deployment 30 percent; state machine functionality restored; multithreading logging verified; altimeter broke and replaced * Stop logging on END state; provide deployment function with AGL instead of ASL altitude * Various minimal changes; Flash size from 1MB to 8MB; M1939 to M2500T burn time; pin assignments for new PCB; External Status LED to Internal Status LED --------- Co-authored-by: Jazz Jackson <[email protected]> Co-authored-by: Cian Capacci <[email protected]> Co-authored-by: Gregory Wainer <[email protected]>
Diffstat (limited to 'include/unused/rocketUtils.hpp')
-rw-r--r--include/unused/rocketUtils.hpp121
1 files changed, 121 insertions, 0 deletions
diff --git a/include/unused/rocketUtils.hpp b/include/unused/rocketUtils.hpp
new file mode 100644
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--- /dev/null
+++ b/include/unused/rocketUtils.hpp
@@ -0,0 +1,121 @@
+#pragma once
+#include <iostream>
+#include <vector>
+#include <ctime>
+#include <vector>
+#include <iomanip>
+#include <sstream>
+#include <fstream>
+
+// Deployment angle limits
+#define MAX_ANGLE 100
+#define MIN_ANGLE 120
+
+// Altimeter initialization count limit
+#define COUNT_LIMIT 50
+
+// Constants
+#define G_0 9.8066
+
+// Threshold limits
+#define BOOST_ACCEL_THRESH 3
+#define BOOST_HEIGHT_THRESH 20
+#define GLIDE_ACCEL_THRESH 0.5
+
+#define ALTI_DEPL_THRESHOLD 0.5
+#define RATE_ALTI_DEPL 1/50
+#define FSM_DONE_SURFACE_ALTITUDE 200
+#define APOGEE_FSM_CHANGE 3
+
+#define INIT_DEPLOYMENT 0
+
+#define TIME_BO 8
+#define TIME_APO 25
+#define TIME_END 120
+
+#define PAD_PRESSURE 102250
+
+#define DUTY_MAX 14.5
+#define DUTY_MIN 3
+
+#define LAUNCH_DATE "4-15-2023"
+#define LOG_FILENAME "DataLog_" LAUNCH_DATE ".txt"
+
+#define LED_GAP_TIME 0.5
+#define LED_ONE_PATH "/sys/class/leds/beaglebone:green:usr1"
+#define LED_BRIGHTNESS_FILE "brightness"
+#define LED_FILENAME LED_ONE_PATH LED_BRIGHTNESS_FILE
+
+#define TEST_MODE false
+
+
+enum VehicleState {ON_PAD, BOOST, GLIDE, APOGEE, DONE};
+extern std::string state_for_log[5];
+
+struct Vehicle {
+
+ int status;
+
+ std::vector<double> acceleration;
+ std::vector<double> linear_acceleration;
+
+ double apogee_altitude;
+ double previous_altitude;
+ double current_altitude;
+ double filtered_altitude;
+
+ double filtered_velocity;
+
+ double deployment_angle;
+
+ bool imuInitFail;
+ bool imuReadFail;
+ bool altiInitFail;
+ bool altiReadFail;
+
+ double ON_PAD_altitude;
+ bool ON_PAD_fail;
+
+ double duty_span;
+
+ double dt;
+
+ int led_brightness;
+
+ time_t start_time;
+ time_t fail_time; // For failure termination
+ time_t liftoff_time;
+ time_t relog_time;
+ time_t deploy_time; // NOT INITIALIZED YET
+ time_t loop_time;
+ time_t led_time;
+};
+
+/**
+ * @brief Convert fin deployment percentage to fin rotation angle
+ *
+ * @param percentage Fin deployment percentage
+ * @return double
+ */
+double deploy_percentage_to_angle(double percentage);
+
+/**
+ * @brief Set the decimal precision of the given data, and return it
+ * as a formatted string with a prefix containing a relevant description of the data.
+ *
+ * @param prefix Identifying or clarifying information about the loggef data
+ * @param data Data to Log
+ * @param precision The decimal precision value for the data
+ *
+ * @return A string with the formatted data.
+ */
+std::string format_data(std::string prefix, double data, int precision);
+
+/**
+ * @brief Blink Beaglebone LED 1
+ *
+ * @param vehicle Holds settings pertinent to the Beaglebone LED
+ * @return true Successful Blink
+ * @return false Unsuccessful Blink
+ */
+bool led_out(Vehicle *vehicle);