Code:
XROM Function Description Input / Output
16,00 -ELLIP APPS Section Header n/a
16,01 BRHM Area of Cyclic Quadrilateral Data in R01-R04
16,02 CIRCLE Circle through three points P1, P2, P3 in Registers R01-R06
16,03 "ECS+" Driver for ECS Prompts for values
16,04 ECS Elliptical Central Sector {a,b,e} in R00-R02, in X
16,05 EFS- Ellliptical Left Focal Sector {a,b,e} in R00-R02, in R03-04
16,06 “EFS+“ Elliptical Right Focal Sector {a,b,e} in R00-R02, in R03-04
16,07 HERON Area of Triangle from sides Data in X,Y,Z
16,08 "F>C“ Focal to Central angles {a,b,e} in R00-R02, in X
16,09 "K2-“ Kepler 2nd. Law – Left Sector Prompts for values
16,10 "K2+“ Kepler 2nd. Law – Right Sector Prompts for values
16,11 "LC0" Central sector Arc Length Prompts for values
16,12 "LF+" Right Focal sectorArc Length Prompts for values
16,13 RAMA2 Ramanujan’s 2nd. Approx. a,b, in Y,X
16,14 ZELIP1 Complex Elliptic Intg. 1st kind z in (Z,Y), m in X
16,15 ZELIP2 Complex Elliptic Intg. 2nd kind z in (Z,Y), m in X
16,16 -ORBITS 101 Section Header n/a
16,17 AZMTH Azimuth angle {a,b,e} in R00-R02, in X
16,18 E>M Eccentric to Mean anomaly (e, E) in Y,X
16,19 E>T Eccentric to True Anomaly (e, E) in Y, X
16,20 M>E Mean to Eccentric anomaly (e, M) in Y,X
16,21 T-E True to Eccentric Anomaly (e, T) in Y,X
16,22 “ORBIT“ Delta-V Orbit Simulator Under program control
16.23 “PRJTL“ Projectile Trajectory Under Program control
16.24 “TA<T>“ True Anomaly via Kepler New Position w/Kepler equation
16.25 “TA+“ True Anomaly Direct Mode (+) New Position using Right sectors
16.26 “TA-“ True Anomaly Direct Mode (-) New Position using Left sectors
16.27 “<)T“ Subroutine for Solve Under program control
16.28 “V<R>“ Velocity “Vis Vivas“ Velocity at distance – Left focus
16.29 “VR+“ Velocity at Position R+ Velocity at distance - right focus
16.30 “VR-“ Velocity at Position R- Velocity at distance - Left focus
16.31 -AUX FNS Section Header n/a
16.32 <)C0+ Central angle for Focal 90° (a b,e) in R00-R02. Lifts stack
16.33 <)C-R Central angle to Radius {a,b,e} in R00-R02, in X
16.34 <)C-XY Central angle to coordinates {a,b,e} in R00-R02, in X
16.35 <)F0+ Right focal angle at x=0 (a,b,e) in R00-R02. Lifts stack
16.36 <)F0- Left Focal angle at x=0 (a,b,e) in R00-R02. Lifts stack
16.37 <)F>R+ Right focal angle to radius {a,b,e} in R00-R02, in X
16.38 <)F>R- Left Focal angle to radius {a,b,e} in R00-R02, in X
16.39 “?ab“ Promptsfor semi-axis New value or R/S for current
16,40 “?<)-“ Prompts for left-angles New value or R/S for current
16,41 “?<)+“ Prompts for right-angles New value or R/S for current
16,42 “?P“ Prompts for Period New value or R/S for current
16,43 1/R^2 Inverse of squared radius {a,b,e} in R00-R02, in X
16,44 QROOT Quadratic Eq. Roots c2, c1, c0 in Z,Y,X
15,45 QROUT Shows roots Roots in X,Y,Z
15.46 THV Tetrahedron Volume Data in R00-R06
15.47 V(X) Velocity at position X Velocity at abccisa - Central
15.48 ZOUT Shows complex value Re,Im in X, Y
15.49 -SOLAR SYS Section Header n/a
15.50 EARTH Planet orbital data Puts data in R00-R02 & R06
15.51 JUPITER Planet orbital data Puts data in R00-R02 & R06
15.52 MARS Planet orbital data Puts data in R00-R02 & R06
15.53 MERCURY Planet orbital data Puts data in R00-R02 & R06
15.54 MOON Satellite orbital data Puts data in R00-R02 & R06
15.55 NEPTUNE Planet orbital data Puts data in R00-R02 & R06
15.56 PLUTO Planet orbital data Puts data in R00-R02 & R06
15.57 SATURN Planet orbital data Puts data in R00-R02 & R06
15.58 URANUS Planet orbital data Puts data in R00-R02 & R06
15.59 VENUS Planet orbital data Puts data in R00-R02 & R06
15.60 +V1 Hohmann Transfer #1 T, R1, R2 in (Z,Y,X)
15,61 +V2 Hohmann Transfer #2 T, R1, R2 in (Z,Y,X)
15,62 1/2 Gravitational Parameter Period in Y, semi-major in X
16,63 T() Period from Gravitational data Mass in Y, semi-major axis in X
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