import mpmath as mp import numba as nb mp.dps = 50 # 设置精度为50位小数 class Orbit: def __init__(self): self.kAlpha = mp.mpf('1.7') / (2 * mp.pi) def InitIdx(self) -> mp.mpf: raise NotImplementedError def InitC(self) -> mp.mpf: raise NotImplementedError def Idx2C(self, idx) -> mp.mpf: raise NotImplementedError def Idx2Cartesian(self, idx) -> [mp.mpf, mp.mpf]: raise NotImplementedError def C2Idx(self, C:[mp.mpf, mp.mpf]) -> mp.mpf: raise NotImplementedError def GenerateNextPointIdx(self, cur_point_idx:mp.mpf, expected_distance:mp.mpf)->mp.mpf: raise NotImplementedError class Loong: def __init__(self, orbit:Orbit, total_points:int, speed:mp.mpf, delta_idx:mp.mpf): self.orbit = orbit self.total_points = total_points self.speed = speed self.delta_idx = delta_idx self.kSegLength1 = mp.mpf('2.86') self.kSegLength2 = mp.mpf('1.65') def CalcStatusListByIdx(self, cur_idx:mp.mpf): first_node_idx=cur_idx first_node_C=self.orbit.Idx2C(first_node_idx) first_node_dot = self.orbit.Idx2Cartesian(first_node_idx) virtual_first_node_idx = first_node_idx + self.delta_idx virtual_first_node_C = self.orbit.Idx2C(virtual_first_node_idx) delta_T = (virtual_first_node_C - first_node_C) / self.speed node_list = [{"idx": first_node_idx, "node": first_node_dot, "C": first_node_C, "v": mp.mpf('1.0')}] for i in range(1, self.total_points): expected_distance = self.kSegLength1 if i == 1 else self.kSegLength2 cur_node_idx = self.orbit.GenerateNextPointIdx(node_list[-1]["idx"], expected_distance) cur_node_dot = self.orbit.Idx2Cartesian(cur_node_idx) cur_node_C = self.orbit.Idx2C(cur_node_idx) virtual_cur_node_idx = self.orbit.GenerateNextPointIdx(virtual_first_node_idx, expected_distance) virtual_cur_node_C = self.orbit.Idx2C(virtual_cur_node_idx) v = (virtual_cur_node_C - cur_node_C) / delta_T node_list.append({"idx": cur_node_idx, "node": cur_node_dot, "C": cur_node_C, "v": v}) virtual_first_node_idx = virtual_cur_node_idx return node_list def CalcStatusListByTime(self, time_point:mp.mpf): first_node_C = self.orbit.InitC() - time_point * self.speed first_node_idx = self.orbit.C2Idx(first_node_C) return self.CalcStatusListByIdx(first_node_idx)