• MikroKopter.de
• Wiki
• SHOP
• Datenschutz
• Impressum

FlightCtrlBL-CtrlMK3MagNaviCtrlProjects

Català-Valencià – Catalan中文 – Chinese (Simplified)中文 – Chinese (Traditional)Česky – CzechDansk – DanishNederlands – DutchEnglish – EnglishSuomi – FinnishFrançais – FrenchDeutsch – Germanעברית – Hebrewहिंदी – HindiMagyar – HungarianBahasa Indonesia – IndonesianItaliano – Italian日本語 – Japanese한국어 – KoreanМакедонски – Macedonianमराठी – MarathiNorsk – NorwegianPolski – PolishPortuguês – PortuguesePortuguês – Portuguese (Brazil)Русский – RussianSlovenčina – SlovakSlovenščina – SlovenianEspañol – SpanishSvenska – SwedishTürkçe – TurkishУкраїнська – UkrainianOëzbekcha – Uzbek

Compare Revisions

• This comparison shows the changes necessary to convert path

  → /branches/dongfang_FC_rewrite/flight.c @ 2058

  → /branches/dongfang_FC_rewrite/flight.c @ 2059

  ↔ Reverse comparison

• Compare Path:	Rev

  With Path:	Rev

Ignore whitespace Rev 2058 → Rev 2059

/branches/dongfang_FC_rewrite/flight.c
135,8 → 135,6
else if (headingError > YAW_I_LIMIT)
headingError = YAW_I_LIMIT;
debugOut.analog[29] = headingError / 100;
PDPart = (int32_t) (headingError * yawIFactor) / (GYRO_DEG_FACTOR_YAW << 4);
// Ehhhhh here is something with desired yaw rate, not?? Ahh OK it gets added in later on.
PDPart += (int32_t) (yawRate * yawPFactor) / (GYRO_DEG_FACTOR_YAW >> 5);