JP 3-50 National Search and Rescue Manual Vol I - US Navy
JP 3-50 National Search and Rescue Manual Vol I - US Navy JP 3-50 National Search and Rescue Manual Vol I - US Navy
fix errors (Fixe) listed in Table 5-2 may be assumed for positions reported as navigation fixes (X=Fixe). If the means of navigation on the distressed craft is unknown, the SMC should assign error on the following basis: a. 5 NM for ships, military submarines, and aircraft with more two engines. b. 10 NM for twin-engine aircraft. c. 15 NM for boats, submersibles, and single-engine aircraft. 2. If the position is determined from an FCC direction-finding network, the fix error corresponds to the assigned classification of the fix as follows: Navigational Fix Errors Class of Fix Fix Error A 20 NM B 40 NM C 60 NM TABLE 5-3. Dead Reckoning Errors Type of Craft DRe Ship 5 percent of the DR distance Submarine (military) 5 percent of the DR distance Aircraft (more than 2 engines) 5 percent of the DR distance Aircraft (twin-engine) 10 percent of the DR distance Aircraft (single-engine) 15 percent of the DR distance Submersible 15 percent of the DR distance Boat 15 percent of the DR distance 3. When the initially reported position is based on dead reckoning (DR), an additional error is assumed for the distance traveled since the last fix. The initial position error is the sum of the fix error and DR error (DRe). Table 5-3 gives DRe which may be assumed for various types of craft. D. SRU Error (Y) based on errors in SRU navigation accuracy, should be considered by the SMC. Since SRUs maintain frequent fixes, usually only Fixe is used. However, if an SRU uses DR navigation in the search area, the SMC should be advised. The SMC then uses both Fixe and
DRe to determine SRU error (Y = Fixe + DRe). E. Total Probable Error (E) is calculated using one of the following formulas: 1. E = X2+Y2 for the initial 4 hours of a mission when drift can be disregarded, and in most inland missions. 2. E = De2+X2+Y2 when drift forces are relevant. F. Recalculation of E is necessary when one of the following happens: 1. The drift changes. A target in water continually drifts. The SMC periodically recomputes datum, leading to a change in De. To illustrate, suppose a surface position is the initially reported position. Drift and drift error are zero. When datum is computed 4 hours later, d1 = 16 miles, and de1 = 4.8 miles, making De = de1 = 4.8 miles. Six hours later datum 2 is computed with d2 = 24 miles and de2 = 7.2 miles, making De = de1 + de2 = 4.8 + 7.2 = 12 miles. The process is continued throughout the mission. 2. The SRUs change. The SMC recomputes E each time the SRU is changed if the Fixe(Y) changes. 3. The initial position changes. Once errors in the initial position are computed, they usually are not changed unless later information shows initial assumptions to be in error. 522 Search Radius The search radius (R) is the radius of a circle centered on a datum, having a length equal to E plus an additional safety length to help ensure that the target is in the search area. For ground and underwater searches, R is measured in yards. On other searches, R is measured in nautical miles. R is usually increased after successive searches to increase the chance of the target being in the search area. Table 5-4 lists Safety Factors (fs) used sequentially to gradually enlarge the search area. TABLE 5-4. Search Radius Safety Factors Search fs 1st 1.1 2nd 1.6 3rd 2.0 4th 2.3 5th 2.5 Subsequent Searches 2.5 5-14
- Page 89 and 90: 3. 2638 kHz, all areas. 4. 2738 kHz
- Page 91 and 92: SRUs and agencies. A search action
- Page 93 and 94: 2. Rescue Area f. SRUs on scene a.
- Page 95 and 96: extended time, a Notice to Mariners
- Page 97 and 98: The receiving and recording of info
- Page 99 and 100: case. The SMC is often automaticall
- Page 101 and 102: any source. b. There is suspicion t
- Page 103 and 104: The craft's float or flight plan is
- Page 105 and 106: Figure 4-1. Water Chill Without Ant
- Page 107 and 108: s Figure 4-2. Wind Chill Graph - Eq
- Page 109 and 110: 445 Weather A. Weather may limit SA
- Page 111 and 112: 451 Uncertainty Phase An Emergency
- Page 113 and 114: 471 PRECOM A. PRECOM search contact
- Page 115 and 116: the objective during their normal o
- Page 117 and 118: effective search plan. The plan may
- Page 119 and 120: D. Other SAR planning models, such
- Page 121 and 122: 1. The aircraft glide area shown in
- Page 123 and 124: Figure 5-3. Vector Plots of Surface
- Page 125 and 126: TABLE 5-1. Parachute Drift Distance
- Page 127 and 128: the search object has, the greater
- Page 129 and 130: B. Sea Current (SC) is the residual
- Page 131 and 132: Figure 5-6A. Wind Current - North L
- Page 133 and 134: large lake can vary with season, we
- Page 135 and 136: 5. Other on scene observations can
- Page 137 and 138: 520 SEARCH AREA Figure 5-8. Minimax
- Page 139: Figure 5-9. Drift Error by Minimax
- Page 143 and 144: Figure 5-11. Search Areas - Moving
- Page 145 and 146: E. When only a datum area exists, s
- Page 147 and 148: SRUs are dispatched next. Supplemen
- Page 149 and 150: B. POD can be increased by decreasi
- Page 151 and 152: C. Visual sweep widths are determin
- Page 153 and 154: TABLE 5-6. Visual Sweep Width Estim
- Page 155 and 156: 9. Fatigue. Degradation of detectio
- Page 157 and 158: Table 5-8. Height of Eye vs. Horizo
- Page 159 and 160: 6. Sweep widths for Side-Looking Ai
- Page 161 and 162: TABLE 5-11a. Sweep Widths for Forwa
- Page 163 and 164: Sweep widths should be approximated
- Page 165 and 166: TABLE 5-14. Environmental Limitatio
- Page 167 and 168: Figure 5-19. Maritime Probability o
- Page 169 and 170: again, unless it is determined furt
- Page 171 and 172: c. This track spacing may exceed th
- Page 173 and 174: a. E-7 corners 23 15N 74 35W to 23
- Page 175 and 176: E. Orienting Search Areas Search pa
- Page 177 and 178: Figure 5-21. Typical Assignments fo
- Page 179 and 180: The major pattern characteristic is
- Page 181 and 182: Figure 5-26. Figure 5-27. 3. Parall
- Page 183 and 184: Figure 5-31. Figure 5-32. D. Creepi
- Page 185 and 186: area, they must fly their individua
- Page 187 and 188: for large objects in well-defined s
- Page 189 and 190: I. Homing Patterns (H) are used to
fix errors (Fixe) listed in Table 5-2 may be assumed for<br />
positions reported as navigation fixes (X=Fixe). If the means<br />
of navigation on the distressed craft is unknown, the SMC<br />
should assign error on the following basis:<br />
a. 5 NM for ships, military submarines, <strong>and</strong> aircraft<br />
with more two engines.<br />
b. 10 NM for twin-engine aircraft.<br />
c. 15 NM for boats, submersibles, <strong>and</strong> single-engine<br />
aircraft.<br />
2. If the position is determined from an FCC direction-finding<br />
network, the fix error corresponds to the assigned<br />
classification of the fix as follows:<br />
Navigational Fix Errors<br />
Class of Fix Fix Error<br />
A 20 NM<br />
B 40 NM<br />
C 60 NM<br />
TABLE 5-3. Dead Reckoning Errors<br />
Type of Craft DRe<br />
Ship 5 percent of the DR distance<br />
Submarine (military) 5 percent of the DR distance<br />
Aircraft (more than 2 engines) 5 percent of the DR distance<br />
Aircraft (twin-engine) 10 percent of the DR distance<br />
Aircraft (single-engine) 15 percent of the DR distance<br />
Submersible 15 percent of the DR distance<br />
Boat 15 percent of the DR distance<br />
3. When the initially reported position is based on dead<br />
reckoning (DR), an additional error is assumed for the<br />
distance traveled since the last fix. The initial position<br />
error is the sum of the fix error <strong>and</strong> DR error (DRe). Table<br />
5-3 gives DRe which may be assumed for various types of craft.<br />
D. SRU Error (Y) based on errors in SRU navigation accuracy,<br />
should be considered by the SMC. Since SRUs maintain frequent fixes,<br />
usually only Fixe is used. However, if an SRU uses DR navigation in the<br />
search area, the SMC should be advised. The SMC then uses both Fixe <strong>and</strong>