1. Enter Altitude in feet and press A. Static pressure is displayed in millibars (mbar). Static temperature is stored in R6
2. Enter Calibrated Airspeed in knots, True Airspeed in knots or Mach, then do one of:
2a. Press B to convert True Airspeed to Mach.
2b. Press C to convert Calibrated Airspeed to Mach.
2c. Press D to convert Mach to True Airspeed.
2d. Press E to convert Mach to Calibrated Airspeed.
2e. Press B then E to convert True Airspeed to Calibrated Airspeed.
2f. Press C then D to convert Calibrated Airspeed to True Airspeed.
Further speed conversions can be made at the same altitude starting from step 2.
Parameters are also stored in R0 to R6.
Copyright (C) 2020 by Alan Waddington
Permission to use, copy, modify, and/or distribute this software for any purpose
with or without fee is hereby granted.
THE SOFTWARE IS PROVIDED "AS IS" AND THE AUTHOR DISCLAIMS ALL WARRANTIES WITH
REGARD TO THIS SOFTWARE INCLUDING ALL IMPLIED WARRANTIES OF MERCHANTABILITY AND
FITNESS. IN NO EVENT SHALL THE AUTHOR BE LIABLE FOR ANY SPECIAL, DIRECT,
INDIRECT, OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER RESULTING FROM LOSS
OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF CONTRACT, NEGLIGENCE OR OTHER
TORTIOUS ACTION, ARISING OUT OF OR IN CONNECTION WITH THE USE OR PERFORMANCE OF
THIS SOFTWARE.
Code: Select all
000 { }
001 { 42 21 11 } f LBL A
002 { 44 0 } STO 0
003 { 3 } 3
004 { 6 } 6
005 { 0 } 0
006 { 8 } 8
007 { 9 } 9
008 { 43 30 8 } g TEST x<y
009 { 22 48 0 } GTO .0
010 { 2 } 2
011 { 8 } 8
012 { 8 } 8
013 { 48 } .
014 { 1 } 1
015 { 5 } 5
016 { 45 0 } RCL 0
017 { 1 } 1
018 { 48 } .
019 { 9 } 9
020 { 8 } 8
021 { 1 } 1
022 { 2 } 2
023 { 26 } EEX
024 { 16 } CHS
025 { 3 } 3
026 { 20 } ×
027 { 30 } −
028 { 44 6 } STO 6
029 { 2 } 2
030 { 8 } 8
031 { 8 } 8
032 { 48 } .
033 { 1 } 1
034 { 5 } 5
035 { 34 } x↔y
036 { 10 } ÷
037 { 5 } 5
038 { 48 } .
039 { 2 } 2
040 { 5 } 5
041 { 5 } 5
042 { 8 } 8
043 { 7 } 7
044 { 9 } 9
045 { 16 } CHS
046 { 14 } yˣ
047 { 1 } 1
048 { 0 } 0
049 { 1 } 1
050 { 3 } 3
051 { 48 } .
052 { 2 } 2
053 { 5 } 5
054 { 20 } ×
055 { 44 4 } STO 4
056 { 43 32 } g RTN
057 { 42 21 48 0 } f LBL .0
058 { 45 0 } RCL 0
059 { 6 } 6
060 { 5 } 5
061 { 6 } 6
062 { 1 } 1
063 { 7 } 7
064 { 43 10 } g x≤y
065 { 22 48 1 } GTO .1
066 { 2 } 2
067 { 1 } 1
068 { 6 } 6
069 { 48 } .
070 { 6 } 6
071 { 5 } 5
072 { 44 6 } STO 6
073 { 2 } 2
074 { 48 } .
075 { 3 } 3
076 { 5 } 5
077 { 4 } 4
078 { 7 } 7
079 { 2 } 2
080 { 9 } 9
081 { 45 0 } RCL 0
082 { 3 } 3
083 { 6 } 6
084 { 0 } 0
085 { 8 } 8
086 { 9 } 9
087 { 30 } −
088 { 2 } 2
089 { 48 } .
090 { 0 } 0
091 { 8 } 8
092 { 7 } 7
093 { 3 } 3
094 { 7 } 7
095 { 26 } EEX
096 { 16 } CHS
097 { 5 } 5
098 { 20 } ×
099 { 30 } −
100 { 13 } 10ˣ
101 { 44 4 } STO 4
102 { 43 32 } g RTN
103 { 42 21 48 1 } f LBL .1
104 { 2 } 2
105 { 1 } 1
106 { 6 } 6
107 { 48 } .
108 { 6 } 6
109 { 5 } 5
110 { 45 0 } RCL 0
111 { 6 } 6
112 { 5 } 5
113 { 6 } 6
114 { 1 } 1
115 { 7 } 7
116 { 30 } −
117 { 0 } 0
118 { 48 } .
119 { 3 } 3
120 { 0 } 0
121 { 4 } 4
122 { 8 } 8
123 { 26 } EEX
124 { 16 } CHS
125 { 3 } 3
126 { 20 } ×
127 { 40 } +
128 { 44 6 } STO 6
129 { 2 } 2
130 { 1 } 1
131 { 6 } 6
132 { 48 } .
133 { 6 } 6
134 { 5 } 5
135 { 34 } x↔y
136 { 10 } ÷
137 { 3 } 3
138 { 4 } 4
139 { 48 } .
140 { 1 } 1
141 { 6 } 6
142 { 3 } 3
143 { 2 } 2
144 { 1 } 1
145 { 5 } 5
146 { 14 } yˣ
147 { 5 } 5
148 { 4 } 4
149 { 48 } .
150 { 7 } 7
151 { 4 } 4
152 { 8 } 8
153 { 2 } 2
154 { 20 } ×
155 { 44 4 } STO 4
156 { 43 32 } g RTN
157 { 42 21 12 } f LBL B
158 { 44 1 } STO 1
159 { 45 6 } RCL 6
160 { 11 } √x̅
161 { 3 } 3
162 { 8 } 8
163 { 48 } .
164 { 9 } 9
165 { 6 } 6
166 { 7 } 7
167 { 8 } 8
168 { 5 } 5
169 { 4 } 4
170 { 20 } ×
171 { 10 } ÷
172 { 44 3 } STO 3
173 { 43 32 } g RTN
174 { 42 21 13 } f LBL C
175 { 32 1 } GSB 1
176 { 32 2 } GSB 2
177 { 43 32 } g RTN
178 { 42 21 1 } f LBL 1
179 { 44 2 } STO 2
180 { 6 } 6
181 { 6 } 6
182 { 1 } 1
183 { 48 } .
184 { 4 } 4
185 { 7 } 7
186 { 8 } 8
187 { 6 } 6
188 { 43 30 8 } g TEST x<y
189 { 22 48 2 } GTO .2
190 { 34 } x↔y
191 { 36 } ENTER
192 { 20 } ×
193 { 4 } 4
194 { 48 } .
195 { 5 } 5
196 { 7 } 7
197 { 0 } 0
198 { 8 } 8
199 { 6 } 6
200 { 5 } 5
201 { 26 } EEX
202 { 7 } 7
203 { 16 } CHS
204 { 20 } ×
205 { 1 } 1
206 { 40 } +
207 { 3 } 3
208 { 48 } .
209 { 5 } 5
210 { 14 } yˣ
211 { 1 } 1
212 { 30 } −
213 { 1 } 1
214 { 0 } 0
215 { 1 } 1
216 { 3 } 3
217 { 48 } .
218 { 2 } 2
219 { 5 } 5
220 { 20 } ×
221 { 43 32 } g RTN
222 { 42 21 48 2 } f LBL .2
223 { 34 } x↔y
224 { 7 } 7
225 { 14 } yˣ
226 { 3 } 3
227 { 48 } .
228 { 0 } 0
229 { 1 } 1
230 { 2 } 2
231 { 3 } 3
232 { 2 } 2
233 { 5 } 5
234 { 5 } 5
235 { 26 } EEX
236 { 1 } 1
237 { 8 } 8
238 { 16 } CHS
239 { 20 } ×
240 { 45 2 } RCL 2
241 { 36 } ENTER
242 { 20 } ×
243 { 1 } 1
244 { 48 } .
245 { 5 } 5
246 { 9 } 9
247 { 9 } 9
248 { 8 } 8
249 { 0 } 0
250 { 2 } 2
251 { 8 } 8
252 { 26 } EEX
253 { 5 } 5
254 { 16 } CHS
255 { 20 } ×
256 { 1 } 1
257 { 30 } −
258 { 2 } 2
259 { 48 } .
260 { 5 } 5
261 { 14 } yˣ
262 { 10 } ÷
263 { 1 } 1
264 { 30 } −
265 { 1 } 1
266 { 0 } 0
267 { 1 } 1
268 { 3 } 3
269 { 48 } .
270 { 2 } 2
271 { 5 } 5
272 { 20 } ×
273 { 43 32 } g RTN
274 { 42 21 2 } f LBL 2
275 { 44 5 } STO 5
276 { 45 4 } RCL 4
277 { 10 } ÷
278 { 1 } 1
279 { 40 } +
280 { 2 } 2
281 { 36 } ENTER
282 { 7 } 7
283 { 10 } ÷
284 { 14 } yˣ
285 { 1 } 1
286 { 30 } −
287 { 5 } 5
288 { 20 } ×
289 { 11 } √x̅
290 { 44 3 } STO 3
291 { 1 } 1
292 { 34 } x↔y
293 { 43 30 8 } g TEST x<y
294 { 43 32 } g RTN
295 { 36 } ENTER
296 { 36 } ENTER
297 { 2 } 2
298 { 40 } +
299 { 42 10 3 } f SOLVE 3
300 { 43 32 } g RTN
301 { 22 0 } GTO 0
302 { 42 21 3 } f LBL 3
303 { 32 4 } GSB 4
304 { 45 5 } RCL 5
305 { 30 } −
306 { 43 32 } g RTN
307 { 42 21 14 } f LBL D
308 { 44 3 } STO 3
309 { 45 6 } RCL 6
310 { 11 } √x̅
311 { 20 } ×
312 { 3 } 3
313 { 8 } 8
314 { 48 } .
315 { 9 } 9
316 { 6 } 6
317 { 7 } 7
318 { 8 } 8
319 { 5 } 5
320 { 4 } 4
321 { 20 } ×
322 { 43 32 } g RTN
323 { 42 21 15 } f LBL E
324 { 32 4 } GSB 4
325 { 32 5 } GSB 5
326 { 43 32 } g RTN
327 { 42 21 4 } f LBL 4
328 { 44 3 } STO 3
329 { 1 } 1
330 { 43 30 8 } g TEST x<y
331 { 22 48 3 } GTO .3
332 { 34 } x↔y
333 { 36 } ENTER
334 { 20 } ×
335 { 0 } 0
336 { 48 } .
337 { 2 } 2
338 { 20 } ×
339 { 1 } 1
340 { 40 } +
341 { 3 } 3
342 { 48 } .
343 { 5 } 5
344 { 14 } yˣ
345 { 1 } 1
346 { 30 } −
347 { 45 4 } RCL 4
348 { 20 } ×
349 { 43 32 } g RTN
350 { 42 21 48 3 } f LBL .3
351 { 34 } x↔y
352 { 7 } 7
353 { 14 } yˣ
354 { 1 } 1
355 { 6 } 6
356 { 6 } 6
357 { 48 } .
358 { 9 } 9
359 { 2 } 2
360 { 1 } 1
361 { 5 } 5
362 { 8 } 8
363 { 20 } ×
364 { 45 3 } RCL 3
365 { 36 } ENTER
366 { 20 } ×
367 { 7 } 7
368 { 20 } ×
369 { 1 } 1
370 { 30 } −
371 { 2 } 2
372 { 48 } .
373 { 5 } 5
374 { 14 } yˣ
375 { 10 } ÷
376 { 1 } 1
377 { 30 } −
378 { 45 4 } RCL 4
379 { 20 } ×
380 { 43 32 } g RTN
381 { 42 21 5 } f LBL 5
382 { 44 5 } STO 5
383 { 1 } 1
384 { 0 } 0
385 { 1 } 1
386 { 3 } 3
387 { 48 } .
388 { 2 } 2
389 { 5 } 5
390 { 10 } ÷
391 { 1 } 1
392 { 40 } +
393 { 2 } 2
394 { 36 } ENTER
395 { 7 } 7
396 { 10 } ÷
397 { 14 } yˣ
398 { 1 } 1
399 { 30 } −
400 { 4 } 4
401 { 48 } .
402 { 5 } 5
403 { 7 } 7
404 { 0 } 0
405 { 8 } 8
406 { 6 } 6
407 { 5 } 5
408 { 26 } EEX
409 { 7 } 7
410 { 16 } CHS
411 { 10 } ÷
412 { 11 } √x̅
413 { 44 2 } STO 2
414 { 6 } 6
415 { 6 } 6
416 { 1 } 1
417 { 48 } .
418 { 4 } 4
419 { 7 } 7
420 { 8 } 8
421 { 6 } 6
422 { 34 } x↔y
423 { 43 30 8 } g TEST x<y
424 { 43 32 } g RTN
425 { 36 } ENTER
426 { 36 } ENTER
427 { 5 } 5
428 { 0 } 0
429 { 40 } +
430 { 42 10 6 } f SOLVE 6
431 { 43 32 } g RTN
432 { 22 0 } GTO 0
433 { 42 21 6 } f LBL 6
434 { 32 1 } GSB 1
435 { 45 5 } RCL 5
436 { 30 } −
437 { 43 32 } g RTN
Code: Select all
# --------------------------------------------
# HEWLETT·PACKARD 15C Simulator program
# Created with version 4.1.00
# --------------------------------------------
#T:Aeronautical Calculations for dm15L
#D:Conversion between True Airspeed, (TAS), Calibrated Airspeed (CAS) and Mach Number (M) for a given Altitude in accordance with BS2G199:1984.
#D:
#D:1. Enter Altitude in feet and press <span class="HP15CfKeyLabel">A</span>. Static pressure is displayed in millibars (mbar). Static temperature is stored in <span class="HP15CRegister">R6</span>
#D:2. Enter Calibrated Airspeed in knots, True Airspeed in knots or Mach, then do one of:
#D:2a. Press <span class="HP15CfKeyLabel">B</span> to convert True Airspeed to Mach.
#D:2b. Press <span class="HP15CfKeyLabel">C</span> to convert Calibrated Airspeed to Mach.
#D:2c. Press <span class="HP15CfKeyLabel">D</span> to convert Mach to True Airspeed.
#D:2d. Press <span class="HP15CfKeyLabel">E</span> to convert Mach to Calibrated Airspeed.
#D:2e. Press <span class="HP15CfKeyLabel">B</span> then <span class="HP15CfKeyLabel">E</span> to convert True Airspeed to Calibrated Airspeed.
#D:2f. Press <span class="HP15CfKeyLabel">C</span> then <span class="HP15CfKeyLabel">D</span> to convert Calibrated Airspeed to True Airspeed.
#D:
#D:Further speed conversions can be made at the same altitude starting from step 2.
#D:
#D:Parameters are also stored in <span class="HP15CRegister">R0</span> to <span class="HP15CRegister">R6</span>.
#D:
#D:Copyright (C) 2020 by Alan Waddington
#D:
#D:Permission to use, copy, modify, and/or distribute this software for any purpose
#D:with or without fee is hereby granted.
#D:
#D:THE SOFTWARE IS PROVIDED "AS IS" AND THE AUTHOR DISCLAIMS ALL WARRANTIES WITH
#D:REGARD TO THIS SOFTWARE INCLUDING ALL IMPLIED WARRANTIES OF MERCHANTABILITY AND
#D:FITNESS. IN NO EVENT SHALL THE AUTHOR BE LIABLE FOR ANY SPECIAL, DIRECT,
#D:INDIRECT, OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER RESULTING FROM LOSS
#D:OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF CONTRACT, NEGLIGENCE OR OTHER
#D:TORTIOUS ACTION, ARISING OUT OF OR IN CONNECTION WITH THE USE OR PERFORMANCE OF
#D:THIS SOFTWARE.
#L-1:Altitude to Static Pressure (Ps)
#L-2:True Airspeed (TAS) to Mach (M)
#L-3:Calibrated Airspeed (CAS) to Mach (M)
#L-4:Mach (M) to True Airspeed (TAS)
#L-5:Mach (M) to Calibrated Airspeed (CAS)
#L0:Generate Error 4 (Solve Failed)
#L1:Calibrated Airspeed (CAS) to Dynamic Pressure (Qc)
#L2:Dynamic Pressure (Qc) to Mach (M)
#L3:SOLVE Equation for supersonic Mach
#L4:Mach (M) to Dynamic Pressure (Qc)
#L5:Dynamic Pressure (Qc) to Calibrated Airspeed (CAS)
#L6:SOLVE Equation for supersonic Calibrated Airspeed
#L10:
#L11:
#L12:
#R0:Altitude (feet)
#R1:True Airspeed (TAS) (knots)
#R2:Calibrated Airspeed (CAS) (knots)
#R3:Mach Number
#R4:Static Pressure (Ps) (mbar)
#R5:Dynamic Pressure (Qc) (mbar)
#R6:Static Temperature (Ts) (K)
# --------------------------------------------
000 { }
001 { 42 21 11 } f LBL A
002 { 44 0 } STO 0
003 { 3 } 3
004 { 6 } 6
005 { 0 } 0
006 { 8 } 8
007 { 9 } 9
008 { 43 30 8 } g TEST x<y
009 { 22 48 0 } GTO .0
010 { 2 } 2
011 { 8 } 8
012 { 8 } 8
013 { 48 } .
014 { 1 } 1
015 { 5 } 5
016 { 45 0 } RCL 0
017 { 1 } 1
018 { 48 } .
019 { 9 } 9
020 { 8 } 8
021 { 1 } 1
022 { 2 } 2
023 { 26 } EEX
024 { 16 } CHS
025 { 3 } 3
026 { 20 } ×
027 { 30 } −
028 { 44 6 } STO 6
029 { 2 } 2
030 { 8 } 8
031 { 8 } 8
032 { 48 } .
033 { 1 } 1
034 { 5 } 5
035 { 34 } x↔y
036 { 10 } ÷
037 { 5 } 5
038 { 48 } .
039 { 2 } 2
040 { 5 } 5
041 { 5 } 5
042 { 8 } 8
043 { 7 } 7
044 { 9 } 9
045 { 16 } CHS
046 { 14 } yˣ
047 { 1 } 1
048 { 0 } 0
049 { 1 } 1
050 { 3 } 3
051 { 48 } .
052 { 2 } 2
053 { 5 } 5
054 { 20 } ×
055 { 44 4 } STO 4
056 { 43 32 } g RTN
057 { 42 21 48 0 } f LBL .0
058 { 45 0 } RCL 0
059 { 6 } 6
060 { 5 } 5
061 { 6 } 6
062 { 1 } 1
063 { 7 } 7
064 { 43 10 } g x≤y
065 { 22 48 1 } GTO .1
066 { 2 } 2
067 { 1 } 1
068 { 6 } 6
069 { 48 } .
070 { 6 } 6
071 { 5 } 5
072 { 44 6 } STO 6
073 { 2 } 2
074 { 48 } .
075 { 3 } 3
076 { 5 } 5
077 { 4 } 4
078 { 7 } 7
079 { 2 } 2
080 { 9 } 9
081 { 45 0 } RCL 0
082 { 3 } 3
083 { 6 } 6
084 { 0 } 0
085 { 8 } 8
086 { 9 } 9
087 { 30 } −
088 { 2 } 2
089 { 48 } .
090 { 0 } 0
091 { 8 } 8
092 { 7 } 7
093 { 3 } 3
094 { 7 } 7
095 { 26 } EEX
096 { 16 } CHS
097 { 5 } 5
098 { 20 } ×
099 { 30 } −
100 { 13 } 10ˣ
101 { 44 4 } STO 4
102 { 43 32 } g RTN
103 { 42 21 48 1 } f LBL .1
104 { 2 } 2
105 { 1 } 1
106 { 6 } 6
107 { 48 } .
108 { 6 } 6
109 { 5 } 5
110 { 45 0 } RCL 0
111 { 6 } 6
112 { 5 } 5
113 { 6 } 6
114 { 1 } 1
115 { 7 } 7
116 { 30 } −
117 { 0 } 0
118 { 48 } .
119 { 3 } 3
120 { 0 } 0
121 { 4 } 4
122 { 8 } 8
123 { 26 } EEX
124 { 16 } CHS
125 { 3 } 3
126 { 20 } ×
127 { 40 } +
128 { 44 6 } STO 6
129 { 2 } 2
130 { 1 } 1
131 { 6 } 6
132 { 48 } .
133 { 6 } 6
134 { 5 } 5
135 { 34 } x↔y
136 { 10 } ÷
137 { 3 } 3
138 { 4 } 4
139 { 48 } .
140 { 1 } 1
141 { 6 } 6
142 { 3 } 3
143 { 2 } 2
144 { 1 } 1
145 { 5 } 5
146 { 14 } yˣ
147 { 5 } 5
148 { 4 } 4
149 { 48 } .
150 { 7 } 7
151 { 4 } 4
152 { 8 } 8
153 { 2 } 2
154 { 20 } ×
155 { 44 4 } STO 4
156 { 43 32 } g RTN
157 { 42 21 12 } f LBL B
158 { 44 1 } STO 1
159 { 45 6 } RCL 6
160 { 11 } √x̅
161 { 3 } 3
162 { 8 } 8
163 { 48 } .
164 { 9 } 9
165 { 6 } 6
166 { 7 } 7
167 { 8 } 8
168 { 5 } 5
169 { 4 } 4
170 { 20 } ×
171 { 10 } ÷
172 { 44 3 } STO 3
173 { 43 32 } g RTN
174 { 42 21 13 } f LBL C
175 { 32 1 } GSB 1
176 { 32 2 } GSB 2
177 { 43 32 } g RTN
178 { 42 21 1 } f LBL 1
179 { 44 2 } STO 2
180 { 6 } 6
181 { 6 } 6
182 { 1 } 1
183 { 48 } .
184 { 4 } 4
185 { 7 } 7
186 { 8 } 8
187 { 6 } 6
188 { 43 30 8 } g TEST x<y
189 { 22 48 2 } GTO .2
190 { 34 } x↔y
191 { 36 } ENTER
192 { 20 } ×
193 { 4 } 4
194 { 48 } .
195 { 5 } 5
196 { 7 } 7
197 { 0 } 0
198 { 8 } 8
199 { 6 } 6
200 { 5 } 5
201 { 26 } EEX
202 { 7 } 7
203 { 16 } CHS
204 { 20 } ×
205 { 1 } 1
206 { 40 } +
207 { 3 } 3
208 { 48 } .
209 { 5 } 5
210 { 14 } yˣ
211 { 1 } 1
212 { 30 } −
213 { 1 } 1
214 { 0 } 0
215 { 1 } 1
216 { 3 } 3
217 { 48 } .
218 { 2 } 2
219 { 5 } 5
220 { 20 } ×
221 { 43 32 } g RTN
222 { 42 21 48 2 } f LBL .2
223 { 34 } x↔y
224 { 7 } 7
225 { 14 } yˣ
226 { 3 } 3
227 { 48 } .
228 { 0 } 0
229 { 1 } 1
230 { 2 } 2
231 { 3 } 3
232 { 2 } 2
233 { 5 } 5
234 { 5 } 5
235 { 26 } EEX
236 { 1 } 1
237 { 8 } 8
238 { 16 } CHS
239 { 20 } ×
240 { 45 2 } RCL 2
241 { 36 } ENTER
242 { 20 } ×
243 { 1 } 1
244 { 48 } .
245 { 5 } 5
246 { 9 } 9
247 { 9 } 9
248 { 8 } 8
249 { 0 } 0
250 { 2 } 2
251 { 8 } 8
252 { 26 } EEX
253 { 5 } 5
254 { 16 } CHS
255 { 20 } ×
256 { 1 } 1
257 { 30 } −
258 { 2 } 2
259 { 48 } .
260 { 5 } 5
261 { 14 } yˣ
262 { 10 } ÷
263 { 1 } 1
264 { 30 } −
265 { 1 } 1
266 { 0 } 0
267 { 1 } 1
268 { 3 } 3
269 { 48 } .
270 { 2 } 2
271 { 5 } 5
272 { 20 } ×
273 { 43 32 } g RTN
274 { 42 21 2 } f LBL 2
275 { 44 5 } STO 5
276 { 45 4 } RCL 4
277 { 10 } ÷
278 { 1 } 1
279 { 40 } +
280 { 2 } 2
281 { 36 } ENTER
282 { 7 } 7
283 { 10 } ÷
284 { 14 } yˣ
285 { 1 } 1
286 { 30 } −
287 { 5 } 5
288 { 20 } ×
289 { 11 } √x̅
290 { 44 3 } STO 3
291 { 1 } 1
292 { 34 } x↔y
293 { 43 30 8 } g TEST x<y
294 { 43 32 } g RTN
295 { 36 } ENTER
296 { 36 } ENTER
297 { 2 } 2
298 { 40 } +
299 { 42 10 3 } f SOLVE 3
300 { 43 32 } g RTN
301 { 22 0 } GTO 0
302 { 42 21 3 } f LBL 3
303 { 32 4 } GSB 4
304 { 45 5 } RCL 5
305 { 30 } −
306 { 43 32 } g RTN
307 { 42 21 14 } f LBL D
308 { 44 3 } STO 3
309 { 45 6 } RCL 6
310 { 11 } √x̅
311 { 20 } ×
312 { 3 } 3
313 { 8 } 8
314 { 48 } .
315 { 9 } 9
316 { 6 } 6
317 { 7 } 7
318 { 8 } 8
319 { 5 } 5
320 { 4 } 4
321 { 20 } ×
322 { 43 32 } g RTN
323 { 42 21 15 } f LBL E
324 { 32 4 } GSB 4
325 { 32 5 } GSB 5
326 { 43 32 } g RTN
327 { 42 21 4 } f LBL 4
328 { 44 3 } STO 3
329 { 1 } 1
330 { 43 30 8 } g TEST x<y
331 { 22 48 3 } GTO .3
332 { 34 } x↔y
333 { 36 } ENTER
334 { 20 } ×
335 { 0 } 0
336 { 48 } .
337 { 2 } 2
338 { 20 } ×
339 { 1 } 1
340 { 40 } +
341 { 3 } 3
342 { 48 } .
343 { 5 } 5
344 { 14 } yˣ
345 { 1 } 1
346 { 30 } −
347 { 45 4 } RCL 4
348 { 20 } ×
349 { 43 32 } g RTN
350 { 42 21 48 3 } f LBL .3
351 { 34 } x↔y
352 { 7 } 7
353 { 14 } yˣ
354 { 1 } 1
355 { 6 } 6
356 { 6 } 6
357 { 48 } .
358 { 9 } 9
359 { 2 } 2
360 { 1 } 1
361 { 5 } 5
362 { 8 } 8
363 { 20 } ×
364 { 45 3 } RCL 3
365 { 36 } ENTER
366 { 20 } ×
367 { 7 } 7
368 { 20 } ×
369 { 1 } 1
370 { 30 } −
371 { 2 } 2
372 { 48 } .
373 { 5 } 5
374 { 14 } yˣ
375 { 10 } ÷
376 { 1 } 1
377 { 30 } −
378 { 45 4 } RCL 4
379 { 20 } ×
380 { 43 32 } g RTN
381 { 42 21 5 } f LBL 5
382 { 44 5 } STO 5
383 { 1 } 1
384 { 0 } 0
385 { 1 } 1
386 { 3 } 3
387 { 48 } .
388 { 2 } 2
389 { 5 } 5
390 { 10 } ÷
391 { 1 } 1
392 { 40 } +
393 { 2 } 2
394 { 36 } ENTER
395 { 7 } 7
396 { 10 } ÷
397 { 14 } yˣ
398 { 1 } 1
399 { 30 } −
400 { 4 } 4
401 { 48 } .
402 { 5 } 5
403 { 7 } 7
404 { 0 } 0
405 { 8 } 8
406 { 6 } 6
407 { 5 } 5
408 { 26 } EEX
409 { 7 } 7
410 { 16 } CHS
411 { 10 } ÷
412 { 11 } √x̅
413 { 44 2 } STO 2
414 { 6 } 6
415 { 6 } 6
416 { 1 } 1
417 { 48 } .
418 { 4 } 4
419 { 7 } 7
420 { 8 } 8
421 { 6 } 6
422 { 34 } x↔y
423 { 43 30 8 } g TEST x<y
424 { 43 32 } g RTN
425 { 36 } ENTER
426 { 36 } ENTER
427 { 5 } 5
428 { 0 } 0
429 { 40 } +
430 { 42 10 6 } f SOLVE 6
431 { 43 32 } g RTN
432 { 22 0 } GTO 0
433 { 42 21 6 } f LBL 6
434 { 32 1 } GSB 1
435 { 45 5 } RCL 5
436 { 30 } −
437 { 43 32 } g RTN
# --------------------------------------------
This post was updated on 9th June 2020 to remove an unused function from the program.