Controller Design-in控制器導入
Define control, power, protection and thermal boundaries before the propulsion architecture is locked.在推進架構定版前，先界定控制、功率、保護與熱邊界。
THRUST · EFFICIENCY · THERMAL
UAV Propulsion無人機推進
Move from controller selection to a measured, high-thrust-density propulsion path.從控制器選型走向可量測的高推力密度推進路徑。
FROM QUESTION TO SYSTEM · 從問題到系統
Three layers into the application.三個層級，進入應用。
Start at the layer that matches today’s engineering uncertainty. Preserve a path toward deeper integration without overstating maturity.從當前工程不確定性所在的層級開始，保留深化整合的路徑，同時維持成熟度邊界。
Motor–Controller Co-design馬達—控制器協同設計
Match electrical behavior and system constraints, then measure thrust, efficiency and temperature.匹配電性與系統限制，再量測推力、效率與溫度。
Flight-system Validation飛行系統驗證
Bring controller, motor and propeller interfaces into a repeatable validation path.將控制器、馬達與螺旋槳介面納入可重複的驗證路徑。
ROBITHRUST · PRODUCT FAMILY
Three propulsion paths.MiniE、P、X 規格與工程實測
Published specifications, test configurations and bench results in one place.整合已公布的完整規格欄位、測試配置與台架結果，供選型及工程評估。
| Specification · 規格 | RobiThrust MiniE | RobiThrust P | RobiThrust X |
|---|---|---|---|
| Positioning · 產品定位 | Light UAV — endurance efficiency and lower weight / 續航效率與減重 | Premium Type I — large-propeller efficiency and sustained output / 大槳效率與持續輸出 | Performance UAV — high thrust and dynamic response / 高推力與高動態 |
| Motor · 馬達廠商與型號 | maxon ECX32 Flat UAV | maxon ECX42 Flat | Racing Electric / 六俊電機 RUM-3848Y |
| Propeller · 螺旋槳配置 | APC 10 × 4.5MR; up to 11 × 5.5MRP / 可延伸 11 × 5.5MRP | FALCON 15 × 6 or 15 × 6E / 或 15 × 6E | 13–15″ or 10 × 5 tri-blade / 或 10 × 5 三葉槳 |
| Bench supply · 台架測試供電 | 16.8 V | 24 V | 44 V |
| Control core · 控制核心 | Robichip Power SoC | Robichip Power SoC | Robichip Power SoC |
| Driver · 驅動版本 | RobiDev D or HD (G1/G2) | RobiDev D or HD (G1/G2) | RobiDev D or HD (G1/G2) |
| Published thrust · 公布推力 | Approx. 673 gf @ 6,800 rpm / 約 673 gf | 1,615 gf @ 5,700 rpm | 982 gf @ 7,300 rpm |
| Published efficiency · 公布效率 | G2 average 11.17 gf/W over 3,100–5,600 rpm / G2 區間平均 | 6.73 gf/W at the reported test point / 公布測試點 | 5.41 gf/W at the reported test point / 公布測試點 |
Source · 資料來源：RobiThrust product specifications, test data and assembly interfaces, CN / EN, updated 8 October 2026, pp. 1–3. / 中英文技術文件，2026 年 10 月 8 日更新，第 1–3 頁。 Source PDFs下載原始文件
ENGINEERING EVIDENCE · 工程實證
Measured with the configuration in view.保留測試條件，理解每一筆數據。
ENDURANCE · 續航效率
RobiThrust MiniE
11.17gf/W · G2 average / 區間平均
maxon ECX32 Flat UAV · APC 10 × 4.5MR · 16.8 V
- Averaging range · 平均工作區間
- 3,100–5,600 rpm
- G2 average · G2 平均效率
- 11.17 gf/W
- Baseline average · 基準平均效率
- 10.51 gf/W
- Maximum measured thrust · 實測最大推力
- Approx. 673 gf @ 6,800 rpm / 約 673 gf
The efficiency average and maximum thrust refer to different operating points. / 平均效率與最大推力對應不同工作點。
SUSTAINED OUTPUT · 持續輸出
RobiThrust P
1,615gf · measured thrust / 實測推力
maxon ECX42 Flat · FALCON 15 × 6 · 24 V
- Maximum measured thrust · 實測最大推力
- 1,615 gf @ 5,700 rpm
- Measured input power · 實測輸入功率
- 240 W @ 24 V
- Reported-point efficiency · 公布測試點效率
- 6.73 gf/W
- Cooling condition · 散熱條件
- Single-side measured / 單側散熱實測
240 W describes the reported bench point, not a continuous power rating. / 240 W 為公布的台架測試點，並非連續額定功率。
DYNAMIC RESPONSE · 高動態
RobiThrust X
982gf · measured thrust / 實測推力
Racing Electric / 六俊電機 RUM-3848Y · 44 V bench / 台架供電
- Measured thrust · 實測推力
- 982 gf @ 7,300 rpm
- Reported-point efficiency · 公布測試點效率
- 5.41 gf/W
- Propeller options · 螺旋槳配置
- 13–15″ or 10 × 5 tri-blade / 或 10 × 5 三葉槳
- Evidence scope · 資料範圍
- Published performance window / 公布性能工作點
The document lists propeller options without identifying the exact propeller at this measured point. / 文件列有槳型選項，未指明此實測點的確切槳型。
Interfaces & validation組裝介面與驗證範圍
Robichip supplies the Power SoC, RobiDev driver version, and power / thermal interface information. Partners supply motors and propellers; the customer supplies the airframe, battery, cover and final mounting interface.Robichip 提供 Power SoC、RobiDev 驅動版本與電源／熱介面資訊；合作商提供馬達與螺旋槳，客戶提供機體、電池、外罩與最終安裝介面。
- Mechanical · 機構： Mounting holes, tolerances, propeller clearance, screws and torque / 安裝孔位、公差、槳葉間隙、螺絲與扭矩。
- Electrical · 電氣： Supply window, polarity, harness, connectors, phase order and rotation / 供電範圍、極性、線束、接頭、相序與旋轉方向。
- Thermal · 熱管理： Contact surface, mounting orientation, propeller airflow, environment and temperature points / 接觸面、安裝方向、槳流、環境與測溫點。
- Traceability · 追溯： Motor / propeller lots, board / driver revisions, first-article and EOL records / 馬達與槳批次、板卡與驅動版本、首件與出廠紀錄。
Dimensions, weight, continuous ratings and environmental limits are not specified in these documents; confirm them for the selected configuration during Design-in.本文件未提供尺寸、重量、連續額定值與環境限制，需於 Design-in 階段依選定配置確認。
TECHNICAL DOCUMENTS · 技術文件
Keep the full engineering reference.中英文 PDF 規格書下載
Both editions include MiniE, P and X specifications, bench data, figures and assembly interfaces. / 兩種語言版本均收錄三款產品規格、實測數據、圖表與組裝介面。
START A DESIGN-IN CONVERSATION · 開始設計導入
Build the UAV Propulsion case around evidence.以實證建立無人機推進案件。
Start with the system, constraint or validation question. RobiChip will help identify the useful scope before a case is opened.從系統、限制條件或驗證問題開始；案件啟動前，先界定最有效的合作範圍。