From 8e3b2934f374dee0c98aad766342a8cde2362ca6 Mon Sep 17 00:00:00 2001
From: "Marek S. Lukasiewicz" <marek@lukasiewicz.tech>
Date: Wed, 17 Dec 2025 15:35:52 +0100
Subject: [PATCH] Display numeric values on PFD

---
 project/instruments/pfd.gd | 16 ++++++++++++----
 1 file changed, 12 insertions(+), 4 deletions(-)

diff --git a/project/instruments/pfd.gd b/project/instruments/pfd.gd
index bd92309..43790a0 100644
--- a/project/instruments/pfd.gd
+++ b/project/instruments/pfd.gd
@@ -25,10 +25,6 @@ extends Node2D
 	set(value):
 		altitude = value
 		var step = 1
-		if value > 49.5:
-			step = 5
-		if value > 99.5:
-			step = 10
 		altitude_label.text = str(int(step * round(value / step)))
 
 @export var climbrate: float = 1000:
@@ -48,3 +44,15 @@ extends Node2D
 func update(aircraft: Transform3D, velocity: Vector3):
 	var godot_euler = aircraft.basis.get_euler()
 	euler_attitude_deg = Vector3(godot_euler.z, -godot_euler.x, -godot_euler.y) * rad_to_deg(1)
+
+	const mps_to_kt = 1.94384
+	var v_local = aircraft.basis.inverse() * velocity
+	airspeed = max(0, v_local.z) * mps_to_kt
+	var v_horizontal = Vector3(velocity.x, 0, velocity.z)
+	groundspeed = v_horizontal.length() * mps_to_kt
+
+	const mps_to_fpm = 196.848
+	climbrate = velocity.y * mps_to_fpm
+
+	const m_to_ft = 3.2808
+	altitude = aircraft.origin.y * m_to_ft