Is parent note Mechanization equations ko padhne se pehle, tumhe har woh symbol apna banana hoga jo woh tumhare samne phenkta hai. Yeh page har ek ko scratch se build karta hai, us order mein jisme woh ek doosre par depend karte hain.
Navigation mein har cheez teen arrows ka ek set hai: "forward kaunsi taraf hai, right kaunsi taraf hai, neeche kaunsi taraf hai". Frame bas un teen arrows ka ek named choice hai.
Hum chaar frames use karte hain. Har ek ko arrows ki ek choti tripod samjho:
Inertial frame (i) — ek tripod jo Earth ke saath spin nahi karta. Yeh door ke taaron ke relative fixed rehta hai. Yeh "honest" frame hai jahan Newton ka law force=mass×acceleration bina corrections ke kaam karta hai.
Earth frame (e) — ek tripod jo planet se chipka hua hai; yeh Earth ke saath din mein ek baar spin karta hai.
Navigation frame (n) — tumhari current jagah par ek tripod jo North, East, Down (NED) ki taraf point karta hai, ek right-handed set (N → E → D). Jab tum travel karte ho, yeh saath saath chalta hai aur dheere dheere tilt hota hai kyunki zameen curve karti hai.
Body frame (b) — vehicle se bolted ek tripod: naak (forward), right wing, pait (neeche), yeh bhi right-handed. IMU yahan rehta hai.
Parent note ωibb aur Cbn jaise symbols se bhara hua hai. Yeh scary lagta hai; yeh actually ek tidy filing system hai.
Recall
ωien mein, do subscripts aur superscript ka matlab kya hai?
Subscripts ie: Earth ka inertial space ke relative rotation. Superscript n: woh numbers nav (NED) axes ke along likhe gaye hain.
Recall
Cbn mein, conversion kis taraf jaati hai?
Body (b, bottom) se nav (n, top) ki taraf: yeh body-frame numbers leta hai aur tumhe nav-frame numbers deta hai.
Bold letters jaise v, f, g vectors ko denote karte hain. Navigation mein hum inhe zyaadatar teen ki stack mein likhte hain:
vn=vNvEvD(velocity North, East, Down).
Is topic ko vectors ki zaroorat hai kyunki velocity, force, aur gravity sabke paas size aur direction dono hain — ek akela number kabhi nahi keh sakta "North-East ki taraf aur thoda neeche 20 m/s".
Spinning ke liye vector kyun? Ek spin ko ek axis (ek direction) aur ek speed dono chahiye. Dono ko ek arrow mein pack karne se hum rotations par arithmetic kar sakte hain. Ek gyroscope ek sensor hai jo exactly yahi output karta hai: ωibb, body ka inertial space ke relative spin, body axes mein likha gaya.
Ek radian natural angle unit hai: radius ke barabar ek arc sweep karo, woh 1 radian hai (≈57.3∘). Hum radians use karte hain kyunki arc-length = radius × angle sirf radians mein cleanly kaam karta hai — aur wahi fact Layer 3 (position) ka poora base hai.
Parent note ka core rule u˙=ω×u hai. Ise padhne ke liye, tumhe cross product chahiye.
Is topic ko yeh kyun chahiye: ek rotating rigid body apne saath attached har arrow ko circle mein le jaata hai. Cross product exactly woh formula hai jo batata hai ki us arrow ka har point kitni tezi se move karta hai. Isliye attitude propagation (Layer 1) isi se bani hai.
Hum cross product ko ek saath teen arrows par apply karna chahte hain (rotation matrix ke teen columns). Ek neat trick "ω ke saath cross" ko ordinary matrix multiply mein badal deti hai.
Bother kyun karo? Kyunki C˙=C[ω×] phir attitude matrix ke saare teen axes ko ek clean line mein handle karta hai.
Picture: Cbn ka har column ek body axis hai (naak, wing, pait) NED numbers mein drawn. Columns padho aur tumhe pata chal jaata hai ki vehicle exactly kaise tilt hua hai.
Do calculus ideas poori recipe ko jodti hain. Dono simple pictures hain.
Yeh mechanization ka dil kyun hai: IMU sirf rates report karta hai (spin rate, aur — gravity fix karne ke baad — acceleration). Orientation, velocity, aur position paane ke liye hum integrate karte hain: rate → total, teen baar. Har integration parent note ki ek "layer" hai (Layer 1, 2, 3).
Do chote rotation vectors ek spinning, curved planet par rehne ke liye correct karte hain.
ωie — Earth-spin rate, Ωe≈7.292×10−5rad/s (ek sidereal day mein ek chakkar). Isliye honest inertial frame aur Earth frame agree nahi karte.
ωen — transport rate: jab tum round Earth par travel karte ho, tumhara local "Down" dheere dheere tip hota hai Earth ke centre ki taraf point karte rehne ke liye. Nav tripod khud rotate karta hai. Iska size speed aur Earth ke radii of curvature par depend karta hai.
Milke yeh Coriolis / transport corrections produce karte hain jo tumhe velocity equation (Layer 2) mein dikhti hain. Deeper story: Coriolis and Centrifugal Effects. IMU box bolted hai ya gimbal par, yeh affect karta hai ki yeh kaise enter hote hain — dekho Strapdown vs Gimbaled INS.