From 06f667a8b3387c808965c22bf166ba09f624850f Mon Sep 17 00:00:00 2001
From: Matthias Grob <maetugr@gmail.com>
Date: Fri, 22 Nov 2019 16:57:20 +0100
Subject: [PATCH] vtol_att_control: convert angle in one line

---
 src/modules/vtol_att_control/tailsitter.cpp | 3 +--
 1 file changed, 1 insertion(+), 2 deletions(-)

diff --git a/src/modules/vtol_att_control/tailsitter.cpp b/src/modules/vtol_att_control/tailsitter.cpp
index e20d415355..fc44ac447b 100644
--- a/src/modules/vtol_att_control/tailsitter.cpp
+++ b/src/modules/vtol_att_control/tailsitter.cpp
@@ -86,8 +86,7 @@ void Tailsitter::update_vtol_state()
 	 * For the backtransition the pitch is controlled in MC mode again and switches to full MC control reaching the sufficient pitch angle.
 	*/
 
-	Eulerf euler = Quatf(_v_att->q);
-	float pitch = euler.theta();
+	float pitch = Eulerf(Quatf(_v_att->q)).theta();
 
 	if (!_attc->is_fixed_wing_requested()) {